-
What is Flight Dynamics? - Derivation of Equations of Motion for an Aircraft
#Aerospace #Engineering #Aircraft #Flight
Hey everyone!
In this video I'm going to be explaning the forces acting on an aircraft, along with deriving the equations of motion. Most college and university textbooks on aerospace engineering derive these equations in a very complicated manner. This video aims to simplify the concepts and intuitively explain flight dynamics.
This video assumes you have a basic understanding of dynamics, vectors, and Newton's Laws of motion, along with yaw, pitch, roll angles
Timestamps:
Recap of Dynamics: 00:30
Aircraft Free Body Diagram: 01:20
Derivation of Force Equations: 02:40
Derivation of Moment Equations: 04:30
Derivation of Rotation Equations: 07:20
Make sure to subscribe for more videos on Mechanical and Aerospace Engineering!
Best wishes,
VDEn...
published: 23 Sep 2019
-
S1 V1: Aircraft Equations of Motion | Forces on Airplane | Flight Dynamics | Flight Mechanics
This is 1st Video of Section 1: Aircraft Equations of Motion. Forces acting on cruise flight.
This is 1st Video of series Flight Dynamics
This videos series in divided into various sections where Section 1 is Cruise Flight Performance
Contents of this video is as following:
1. In this video basic four forces acting on airplane during cruise flight are explained.
These four forces are Lift, Drag, Thrust and Weight.
2. Equations of motion is developed for simple cruise case.
3. The case for accelerated flight without gaining altitude is also discussed and equations of motions are then developed for this case.
4. Formula for lift and drag is also explained.
5. Case for climbing flight is discussed.
6. Equations of motion for climbing flight is also discussed.
published: 27 Mar 2020
-
Aircraft Dynamics . Equations of Motion . 6 DOF Equations of Motion Summary
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community! Learn more at https://www.aero-academy.org/
published: 08 Mar 2021
-
A Nonlinear, 6 DOF Dynamic Model of an Aircraft: the Research Civil Aircraft Model (RCAM)
In this video we develop a dynamic model of an aircraft by describing forces and moments generated by aerodynamic, propulsion, and gravity that act on the aircraft. This video outlines the analytical models/equations used as well as provides some discussion on the features and phenomenon that are captured in the RCAM model. A separate video discusses how to implement this in Matlab/Simulink.
This model is based on the Research Civil Aircraft Model (RCAM) documented in the following reference:
-Group for Aeronautical Research and Technology in Europe, "Robust Flight Control Design Challenge Problem Formulation and Manual: the Research Civil Aircraft Model (RCAM)", GARTEUR/TP-0883. February 17, 1997 (https://garteur.org) (an older version of the document is located at https://garteur.or...
published: 26 Apr 2020
-
Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft
#SimulinkChallenge2019 #Matlab #Flight
Files: https://github.com/Vinayak-D/F-16-Longitudinal
My entry to the Simulink Student Challenge 2019
Longitudinal Nonlinear Flight Dynamics and Control of an unstable Fighter Aircraft.
The equations of motion, stability derivatives, aerodynamic coefficients for a longitudinal motion of an aircraft are all computed using Simulink which provides quick turnaround time.
A linearized MIMO state space model is then developed using PID Loops to control both speed and pitch angle simultaneously
Source:
https://dept.aem.umn.edu/~balas/darpa_sec/SEC.Accom.html
Thank you for your consideration
published: 26 Nov 2019
-
The Aerodynamics of Flight
The creator of this video allows full use of its contents for educational purposes.
http://geardownfs.com/
http://twitter.com/geardownfs
This video covers the basic aerodynamics that allow for all different types of aircraft to fly.
Everything in this video should only be applied in theory flight simulation. I am not a real world pilot, and therefore cannot testify on behalf of the actual processes of real world aviation.
Produced by Garth, with GearDownFS
published: 10 Aug 2009
-
Airplane design #2 - Flight Dynamics
For more information, visit https://www.airshaper.com
----------------------------------------------------------------------------------------
In this video, we’ll be discussing the basics of flight dynamics.
1. Introduction
To fly an airplane in a straight leveled line involves a horizontal balance between aerodynamic drag & thrust force and a vertical balance between aerodynamic lift and gravity. To make an airplane take off, follow curved trajectories and land, involves a whole lot more and is the domain of flight dynamics.
2. Roll, Pitch, and Yaw
The main parameters used to describe this three-dimensional orientation are the roll, pitch and yaw axes of the plane, all running through the center of gravity.
- The roll axis, also called the longitudinal axis, runs from nose to
tail...
published: 05 Mar 2019
-
2. Airplane Aerodynamics
MIT 16.687 Private Pilot Ground School, IAP 2019
Instructor: Philip Greenspun, Tina Srivastava
View the complete course: https://ocw.mit.edu/16-687IAP19
YouTube Playlist: https://www.youtube.com/playlist?list=PLUl4u3cNGP63cUdAG3v311Vl72ozOiK25
This lecture introduced the fundamental knowledge and basic principles of airplane aerodynamics.
License: Creative Commons BY-NC-SA
More information at https://ocw.mit.edu/terms
More courses at https://ocw.mit.edu
published: 27 Apr 2020
-
Aerodynamics Explained by a World Record Paper Airplane Designer | Level Up | WIRED
John Collins, origami enthusiast and paper airplane savant, walks us through all the science behind five spectacular paper airplanes. Most people know how to fold a simple plane, but paper airplanes can take as much from science as the newest car designs.
Still haven’t subscribed to WIRED on YouTube? ►► http://wrd.cm/15fP7B7
Listen to the Get WIRED podcast ►► https://link.chtbl.com/wired-ytc-desc
Get more incredible stories on science and tech with our daily newsletter: https://wrd.cm/DailyYT
Also, check out the free WIRED channel on Roku, Apple TV, Amazon Fire TV, and Android TV. Here you can find your favorite WIRED shows and new episodes of our latest hit series Tradecraft.
ABOUT WIRED
WIRED is where tomorrow is realized. Through thought-provoking stories and videos, WIRED...
published: 13 Oct 2020
-
Aircraft Dynamics . Equations of Motion . Position and Orientation - Euler Angles
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community! Learn more at https://www.aero-academy.org/
At 4:23 I said z-axis, but meant x-axis.
published: 05 Mar 2021
11:06
What is Flight Dynamics? - Derivation of Equations of Motion for an Aircraft
#Aerospace #Engineering #Aircraft #Flight
Hey everyone!
In this video I'm going to be explaning the forces acting on an aircraft, along with deriving the equa...
#Aerospace #Engineering #Aircraft #Flight
Hey everyone!
In this video I'm going to be explaning the forces acting on an aircraft, along with deriving the equations of motion. Most college and university textbooks on aerospace engineering derive these equations in a very complicated manner. This video aims to simplify the concepts and intuitively explain flight dynamics.
This video assumes you have a basic understanding of dynamics, vectors, and Newton's Laws of motion, along with yaw, pitch, roll angles
Timestamps:
Recap of Dynamics: 00:30
Aircraft Free Body Diagram: 01:20
Derivation of Force Equations: 02:40
Derivation of Moment Equations: 04:30
Derivation of Rotation Equations: 07:20
Make sure to subscribe for more videos on Mechanical and Aerospace Engineering!
Best wishes,
VDEngineering
My Instagram: http://instagram.com/vinayak_desh
https://wn.com/What_Is_Flight_Dynamics_Derivation_Of_Equations_Of_Motion_For_An_Aircraft
#Aerospace #Engineering #Aircraft #Flight
Hey everyone!
In this video I'm going to be explaning the forces acting on an aircraft, along with deriving the equations of motion. Most college and university textbooks on aerospace engineering derive these equations in a very complicated manner. This video aims to simplify the concepts and intuitively explain flight dynamics.
This video assumes you have a basic understanding of dynamics, vectors, and Newton's Laws of motion, along with yaw, pitch, roll angles
Timestamps:
Recap of Dynamics: 00:30
Aircraft Free Body Diagram: 01:20
Derivation of Force Equations: 02:40
Derivation of Moment Equations: 04:30
Derivation of Rotation Equations: 07:20
Make sure to subscribe for more videos on Mechanical and Aerospace Engineering!
Best wishes,
VDEngineering
My Instagram: http://instagram.com/vinayak_desh
- published: 23 Sep 2019
- views: 7380
6:22
S1 V1: Aircraft Equations of Motion | Forces on Airplane | Flight Dynamics | Flight Mechanics
This is 1st Video of Section 1: Aircraft Equations of Motion. Forces acting on cruise flight.
This is 1st Video of series Flight Dynamics
This videos series in ...
This is 1st Video of Section 1: Aircraft Equations of Motion. Forces acting on cruise flight.
This is 1st Video of series Flight Dynamics
This videos series in divided into various sections where Section 1 is Cruise Flight Performance
Contents of this video is as following:
1. In this video basic four forces acting on airplane during cruise flight are explained.
These four forces are Lift, Drag, Thrust and Weight.
2. Equations of motion is developed for simple cruise case.
3. The case for accelerated flight without gaining altitude is also discussed and equations of motions are then developed for this case.
4. Formula for lift and drag is also explained.
5. Case for climbing flight is discussed.
6. Equations of motion for climbing flight is also discussed.
https://wn.com/S1_V1_Aircraft_Equations_Of_Motion_|_Forces_On_Airplane_|_Flight_Dynamics_|_Flight_Mechanics
This is 1st Video of Section 1: Aircraft Equations of Motion. Forces acting on cruise flight.
This is 1st Video of series Flight Dynamics
This videos series in divided into various sections where Section 1 is Cruise Flight Performance
Contents of this video is as following:
1. In this video basic four forces acting on airplane during cruise flight are explained.
These four forces are Lift, Drag, Thrust and Weight.
2. Equations of motion is developed for simple cruise case.
3. The case for accelerated flight without gaining altitude is also discussed and equations of motions are then developed for this case.
4. Formula for lift and drag is also explained.
5. Case for climbing flight is discussed.
6. Equations of motion for climbing flight is also discussed.
- published: 27 Mar 2020
- views: 773
13:13
Aircraft Dynamics . Equations of Motion . 6 DOF Equations of Motion Summary
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community!...
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community! Learn more at https://www.aero-academy.org/
https://wn.com/Aircraft_Dynamics_._Equations_Of_Motion_._6_Dof_Equations_Of_Motion_Summary
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community! Learn more at https://www.aero-academy.org/
- published: 08 Mar 2021
- views: 753
1:43:33
A Nonlinear, 6 DOF Dynamic Model of an Aircraft: the Research Civil Aircraft Model (RCAM)
In this video we develop a dynamic model of an aircraft by describing forces and moments generated by aerodynamic, propulsion, and gravity that act on the aircr...
In this video we develop a dynamic model of an aircraft by describing forces and moments generated by aerodynamic, propulsion, and gravity that act on the aircraft. This video outlines the analytical models/equations used as well as provides some discussion on the features and phenomenon that are captured in the RCAM model. A separate video discusses how to implement this in Matlab/Simulink.
This model is based on the Research Civil Aircraft Model (RCAM) documented in the following reference:
-Group for Aeronautical Research and Technology in Europe, "Robust Flight Control Design Challenge Problem Formulation and Manual: the Research Civil Aircraft Model (RCAM)", GARTEUR/TP-0883. February 17, 1997 (https://garteur.org) (an older version of the document is located at https://garteur.org/wp-content/reports/FM/FM_AG-08_TP-088-3.pdf)
Topics and timestamps:
0:00 – Introduction to the RCAM model
6:48 – Step 1: Control limits/saturation
11:22 – Step 2: Intermediate variables
23:14 – Step 3: Nondimensional aerodynamic force coefficients in Fs
1:00:24 – Step 4: Aerodynamic force in Fb
1:03:31 – Step 5: Nondimensional aerodynamic moment coefficients about AC in Fb
1:14:12 – Step 6: Aerodynamic moment about AC in Fb
1:16:21 – Step 7: Aerodynamic moment about CG in Fb
1:22:41 – Step 8: Propulsion effects
1:31:08 – Step 9: Gravity effects
1:36:15 – Step 10: Explicit first order form
Errata/Corrections
(38:45) – This is improperly written as +11.5 deg, it should be -11.5 deg
All Flight Mechanics videos in a single playlist (https://www.youtube.com/playlist?list=PLxdnSsBqCrrEx3A6W94sQGClk6Q4YCg-h)
#FlightMechanics
https://wn.com/A_Nonlinear,_6_Dof_Dynamic_Model_Of_An_Aircraft_The_Research_Civil_Aircraft_Model_(Rcam)
In this video we develop a dynamic model of an aircraft by describing forces and moments generated by aerodynamic, propulsion, and gravity that act on the aircraft. This video outlines the analytical models/equations used as well as provides some discussion on the features and phenomenon that are captured in the RCAM model. A separate video discusses how to implement this in Matlab/Simulink.
This model is based on the Research Civil Aircraft Model (RCAM) documented in the following reference:
-Group for Aeronautical Research and Technology in Europe, "Robust Flight Control Design Challenge Problem Formulation and Manual: the Research Civil Aircraft Model (RCAM)", GARTEUR/TP-0883. February 17, 1997 (https://garteur.org) (an older version of the document is located at https://garteur.org/wp-content/reports/FM/FM_AG-08_TP-088-3.pdf)
Topics and timestamps:
0:00 – Introduction to the RCAM model
6:48 – Step 1: Control limits/saturation
11:22 – Step 2: Intermediate variables
23:14 – Step 3: Nondimensional aerodynamic force coefficients in Fs
1:00:24 – Step 4: Aerodynamic force in Fb
1:03:31 – Step 5: Nondimensional aerodynamic moment coefficients about AC in Fb
1:14:12 – Step 6: Aerodynamic moment about AC in Fb
1:16:21 – Step 7: Aerodynamic moment about CG in Fb
1:22:41 – Step 8: Propulsion effects
1:31:08 – Step 9: Gravity effects
1:36:15 – Step 10: Explicit first order form
Errata/Corrections
(38:45) – This is improperly written as +11.5 deg, it should be -11.5 deg
All Flight Mechanics videos in a single playlist (https://www.youtube.com/playlist?list=PLxdnSsBqCrrEx3A6W94sQGClk6Q4YCg-h)
#FlightMechanics
- published: 26 Apr 2020
- views: 12084
5:01
Flight Dynamics Modeling, Linearization & Control of an Unstable Aircraft
#SimulinkChallenge2019 #Matlab #Flight
Files: https://github.com/Vinayak-D/F-16-Longitudinal
My entry to the Simulink Student Challenge 2019
Longitudinal Non...
#SimulinkChallenge2019 #Matlab #Flight
Files: https://github.com/Vinayak-D/F-16-Longitudinal
My entry to the Simulink Student Challenge 2019
Longitudinal Nonlinear Flight Dynamics and Control of an unstable Fighter Aircraft.
The equations of motion, stability derivatives, aerodynamic coefficients for a longitudinal motion of an aircraft are all computed using Simulink which provides quick turnaround time.
A linearized MIMO state space model is then developed using PID Loops to control both speed and pitch angle simultaneously
Source:
https://dept.aem.umn.edu/~balas/darpa_sec/SEC.Accom.html
Thank you for your consideration
https://wn.com/Flight_Dynamics_Modeling,_Linearization_Control_Of_An_Unstable_Aircraft
#SimulinkChallenge2019 #Matlab #Flight
Files: https://github.com/Vinayak-D/F-16-Longitudinal
My entry to the Simulink Student Challenge 2019
Longitudinal Nonlinear Flight Dynamics and Control of an unstable Fighter Aircraft.
The equations of motion, stability derivatives, aerodynamic coefficients for a longitudinal motion of an aircraft are all computed using Simulink which provides quick turnaround time.
A linearized MIMO state space model is then developed using PID Loops to control both speed and pitch angle simultaneously
Source:
https://dept.aem.umn.edu/~balas/darpa_sec/SEC.Accom.html
Thank you for your consideration
- published: 26 Nov 2019
- views: 5004
7:14
The Aerodynamics of Flight
The creator of this video allows full use of its contents for educational purposes.
http://geardownfs.com/
http://twitter.com/geardownfs
This video covers th...
The creator of this video allows full use of its contents for educational purposes.
http://geardownfs.com/
http://twitter.com/geardownfs
This video covers the basic aerodynamics that allow for all different types of aircraft to fly.
Everything in this video should only be applied in theory flight simulation. I am not a real world pilot, and therefore cannot testify on behalf of the actual processes of real world aviation.
Produced by Garth, with GearDownFS
https://wn.com/The_Aerodynamics_Of_Flight
The creator of this video allows full use of its contents for educational purposes.
http://geardownfs.com/
http://twitter.com/geardownfs
This video covers the basic aerodynamics that allow for all different types of aircraft to fly.
Everything in this video should only be applied in theory flight simulation. I am not a real world pilot, and therefore cannot testify on behalf of the actual processes of real world aviation.
Produced by Garth, with GearDownFS
- published: 10 Aug 2009
- views: 2120995
4:36
Airplane design #2 - Flight Dynamics
For more information, visit https://www.airshaper.com
----------------------------------------------------------------------------------------
In this video, w...
For more information, visit https://www.airshaper.com
----------------------------------------------------------------------------------------
In this video, we’ll be discussing the basics of flight dynamics.
1. Introduction
To fly an airplane in a straight leveled line involves a horizontal balance between aerodynamic drag & thrust force and a vertical balance between aerodynamic lift and gravity. To make an airplane take off, follow curved trajectories and land, involves a whole lot more and is the domain of flight dynamics.
2. Roll, Pitch, and Yaw
The main parameters used to describe this three-dimensional orientation are the roll, pitch and yaw axes of the plane, all running through the center of gravity.
- The roll axis, also called the longitudinal axis, runs from nose to
tail.
- The pitch axis, also called the transverse axis, runs from left to
right.
- The yaw axis, also called the vertical axis, runs from top to
bottom.
Also important is the plane’s orientation with respect to the relative wind vector, which is the combination of the velocity vector of the plane and the wind vector. Around the pitch axis, this is called the angle of attack. Around the yaw axis, this is called the sideslip angle.
3. Leveled flight
During a leveled flight, the roll, pitch & yaw orientation stay constant. To achieve this static balance, the moments around all three axes must be zero, otherwise, the plane would start to change its orientation.
For example, if the center of lift of the main wings is not aligned with the center of gravity, this can generate a pitch moment causing the plane to tilt its nose upward or downward. To neutralize this pitch-moment, lift or downforce can be generated at the tail. Keep in mind that the location of the center of gravity can change between flights and even during flights due to changes in cargo and fuel for example.
4. Dynamic flight
During dynamic flight maneuvers, the airplane changes its orientation.
To climb or descend, for example, the elevators at the tail can be lowered or raised. This will cause the angle of attack to change which will affect the lift and drag that are generated on the main wings for example. Mapping & understanding the correlation between angle of attack and lift is crucial to understanding & optimizing flight dynamics.
To achieve this, you can perform a wind tunnel test during which you monitor lift & drag values while gradually increasing the angle of attack from the lowest to the highest value of interest. Such a sweep procedure can also be performed digitally by changing the angle of attack over a series of aerodynamic simulations.
5. Horizontal sweep
The results are curves that plot the lift and drag values versus the angle of attack. This is quite similar to the 2D airfoil curves we saw in earlier videos, only now it’s the lift & drag of the full plane, taking aerodynamic effects like flow around the fuselage and wingtip vortices into account.
Here as well, very steep curves could indicate that the plane is very dynamic but more difficult to fly. Such crucial information can then be used as input for the flight control strategy.
6. Vertical sweep
A similar approach can be applied to a yaw maneuver, where the rudder at the tail is used to turn the plane left or right. Sweeping the sideslip angle beta again results in changes in the forces on the plane. In this case, however, the lateral force is of particular interest, as a sideslip angle will generate a sideways push on the plane.
7.
This is only the tip of the iceberg in terms of flight dynamics: much of the airplane maneuvers involve a combination of pitch, roll, and yaw. Side winds can have a tremendous impact as well. And the speed of rolling, pitching and yawing also generates additional dynamic forces and moments that play a big role.
That was it for this short introduction on flight dynamics. Thanks for liking, sharing and leaving your comments below the video, thanks for watching and see you soon! Bye-bye.
-----------------------------------------------------------------------------------------------------------
Wouter Remmerie
Wouter is the Founder of AirShaper, an online, virtual wind tunnel. With this tool and these videos, we want to make aerodynamics accessible to everyone! Interested in more content like this on the field of aerodynamics? Make sure to click that subscribe button, we post new videos every week!
For more information, visit:
www.airshaper.com
www.facebook.com/AirShaper
www.linkedin.com/company/airshaper
#AirShaper #FlightDynamics #FlightDynamicsAirplanes
https://wn.com/Airplane_Design_2_Flight_Dynamics
For more information, visit https://www.airshaper.com
----------------------------------------------------------------------------------------
In this video, we’ll be discussing the basics of flight dynamics.
1. Introduction
To fly an airplane in a straight leveled line involves a horizontal balance between aerodynamic drag & thrust force and a vertical balance between aerodynamic lift and gravity. To make an airplane take off, follow curved trajectories and land, involves a whole lot more and is the domain of flight dynamics.
2. Roll, Pitch, and Yaw
The main parameters used to describe this three-dimensional orientation are the roll, pitch and yaw axes of the plane, all running through the center of gravity.
- The roll axis, also called the longitudinal axis, runs from nose to
tail.
- The pitch axis, also called the transverse axis, runs from left to
right.
- The yaw axis, also called the vertical axis, runs from top to
bottom.
Also important is the plane’s orientation with respect to the relative wind vector, which is the combination of the velocity vector of the plane and the wind vector. Around the pitch axis, this is called the angle of attack. Around the yaw axis, this is called the sideslip angle.
3. Leveled flight
During a leveled flight, the roll, pitch & yaw orientation stay constant. To achieve this static balance, the moments around all three axes must be zero, otherwise, the plane would start to change its orientation.
For example, if the center of lift of the main wings is not aligned with the center of gravity, this can generate a pitch moment causing the plane to tilt its nose upward or downward. To neutralize this pitch-moment, lift or downforce can be generated at the tail. Keep in mind that the location of the center of gravity can change between flights and even during flights due to changes in cargo and fuel for example.
4. Dynamic flight
During dynamic flight maneuvers, the airplane changes its orientation.
To climb or descend, for example, the elevators at the tail can be lowered or raised. This will cause the angle of attack to change which will affect the lift and drag that are generated on the main wings for example. Mapping & understanding the correlation between angle of attack and lift is crucial to understanding & optimizing flight dynamics.
To achieve this, you can perform a wind tunnel test during which you monitor lift & drag values while gradually increasing the angle of attack from the lowest to the highest value of interest. Such a sweep procedure can also be performed digitally by changing the angle of attack over a series of aerodynamic simulations.
5. Horizontal sweep
The results are curves that plot the lift and drag values versus the angle of attack. This is quite similar to the 2D airfoil curves we saw in earlier videos, only now it’s the lift & drag of the full plane, taking aerodynamic effects like flow around the fuselage and wingtip vortices into account.
Here as well, very steep curves could indicate that the plane is very dynamic but more difficult to fly. Such crucial information can then be used as input for the flight control strategy.
6. Vertical sweep
A similar approach can be applied to a yaw maneuver, where the rudder at the tail is used to turn the plane left or right. Sweeping the sideslip angle beta again results in changes in the forces on the plane. In this case, however, the lateral force is of particular interest, as a sideslip angle will generate a sideways push on the plane.
7.
This is only the tip of the iceberg in terms of flight dynamics: much of the airplane maneuvers involve a combination of pitch, roll, and yaw. Side winds can have a tremendous impact as well. And the speed of rolling, pitching and yawing also generates additional dynamic forces and moments that play a big role.
That was it for this short introduction on flight dynamics. Thanks for liking, sharing and leaving your comments below the video, thanks for watching and see you soon! Bye-bye.
-----------------------------------------------------------------------------------------------------------
Wouter Remmerie
Wouter is the Founder of AirShaper, an online, virtual wind tunnel. With this tool and these videos, we want to make aerodynamics accessible to everyone! Interested in more content like this on the field of aerodynamics? Make sure to click that subscribe button, we post new videos every week!
For more information, visit:
www.airshaper.com
www.facebook.com/AirShaper
www.linkedin.com/company/airshaper
#AirShaper #FlightDynamics #FlightDynamicsAirplanes
- published: 05 Mar 2019
- views: 6562
1:12:07
2. Airplane Aerodynamics
MIT 16.687 Private Pilot Ground School, IAP 2019
Instructor: Philip Greenspun, Tina Srivastava
View the complete course: https://ocw.mit.edu/16-687IAP19
YouTube...
MIT 16.687 Private Pilot Ground School, IAP 2019
Instructor: Philip Greenspun, Tina Srivastava
View the complete course: https://ocw.mit.edu/16-687IAP19
YouTube Playlist: https://www.youtube.com/playlist?list=PLUl4u3cNGP63cUdAG3v311Vl72ozOiK25
This lecture introduced the fundamental knowledge and basic principles of airplane aerodynamics.
License: Creative Commons BY-NC-SA
More information at https://ocw.mit.edu/terms
More courses at https://ocw.mit.edu
https://wn.com/2._Airplane_Aerodynamics
MIT 16.687 Private Pilot Ground School, IAP 2019
Instructor: Philip Greenspun, Tina Srivastava
View the complete course: https://ocw.mit.edu/16-687IAP19
YouTube Playlist: https://www.youtube.com/playlist?list=PLUl4u3cNGP63cUdAG3v311Vl72ozOiK25
This lecture introduced the fundamental knowledge and basic principles of airplane aerodynamics.
License: Creative Commons BY-NC-SA
More information at https://ocw.mit.edu/terms
More courses at https://ocw.mit.edu
- published: 27 Apr 2020
- views: 868464
16:36
Aerodynamics Explained by a World Record Paper Airplane Designer | Level Up | WIRED
John Collins, origami enthusiast and paper airplane savant, walks us through all the science behind five spectacular paper airplanes. Most people know how to fo...
John Collins, origami enthusiast and paper airplane savant, walks us through all the science behind five spectacular paper airplanes. Most people know how to fold a simple plane, but paper airplanes can take as much from science as the newest car designs.
Still haven’t subscribed to WIRED on YouTube? ►► http://wrd.cm/15fP7B7
Listen to the Get WIRED podcast ►► https://link.chtbl.com/wired-ytc-desc
Get more incredible stories on science and tech with our daily newsletter: https://wrd.cm/DailyYT
Also, check out the free WIRED channel on Roku, Apple TV, Amazon Fire TV, and Android TV. Here you can find your favorite WIRED shows and new episodes of our latest hit series Tradecraft.
ABOUT WIRED
WIRED is where tomorrow is realized. Through thought-provoking stories and videos, WIRED explores the future of business, innovation, and culture.
Aerodynamics Explained by a World Record Paper Airplane Designer | Level Up | WIRED
https://wn.com/Aerodynamics_Explained_By_A_World_Record_Paper_Airplane_Designer_|_Level_Up_|_Wired
John Collins, origami enthusiast and paper airplane savant, walks us through all the science behind five spectacular paper airplanes. Most people know how to fold a simple plane, but paper airplanes can take as much from science as the newest car designs.
Still haven’t subscribed to WIRED on YouTube? ►► http://wrd.cm/15fP7B7
Listen to the Get WIRED podcast ►► https://link.chtbl.com/wired-ytc-desc
Get more incredible stories on science and tech with our daily newsletter: https://wrd.cm/DailyYT
Also, check out the free WIRED channel on Roku, Apple TV, Amazon Fire TV, and Android TV. Here you can find your favorite WIRED shows and new episodes of our latest hit series Tradecraft.
ABOUT WIRED
WIRED is where tomorrow is realized. Through thought-provoking stories and videos, WIRED explores the future of business, innovation, and culture.
Aerodynamics Explained by a World Record Paper Airplane Designer | Level Up | WIRED
- published: 13 Oct 2020
- views: 818578
27:37
Aircraft Dynamics . Equations of Motion . Position and Orientation - Euler Angles
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community!...
Free courses, more videos, practice exercises, and sample code available at https://www.aero-academy.org/
Come check it out and join the AeroAcademy community! Learn more at https://www.aero-academy.org/
At 4:23 I said z-axis, but meant x-axis.
https://wn.com/Aircraft_Dynamics_._Equations_Of_Motion_._Position_And_Orientation_Euler_Angles
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At 4:23 I said z-axis, but meant x-axis.
- published: 05 Mar 2021
- views: 514