Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Force  





2 See also  





3 References  














Aerodynamic force






العربية
Беларуская
Español
Հայերեն
ि
Oʻzbekcha / ўзбекча
Polski
Português
Shqip
Slovenčina
Türkçe
Українська
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


The aerodynamic force is the resultant vector from adding the lift vector, perpendicular to the flow direction, and the drag vector, parallel to the flow direction.
Forces on an aerofoil.

Influid mechanics, an aerodynamic force is a force exerted on a body by the air (or other gas) in which the body is immersed, and is due to the relative motion between the body and the gas.

Force[edit]

There are two causes of aerodynamic force: [1]: §4.10 [2][3]: 29 

Pressure acts normal to the surface, and shear force acts parallel to the surface. Both forces act locally. The net aerodynamic force on the body is equal to the pressure and shear forces integrated over the body's total exposed area.[4]

When an airfoil moves relative to the air, it generates an aerodynamic force determined by the velocity of relative motion, and the angle of attack. This aerodynamic force is commonly resolved into two components, both acting through the center of pressure:[3]: 14 [1]: § 5.3 

In addition to these two forces, the body may experience an aerodynamic moment.

The force created by propellers and jet engines is called thrust, and is also an aerodynamic force (since it acts on the surrounding air). The aerodynamic force on a powered airplane is commonly represented by three vectors: thrust, lift and drag.[3]: 151 [1]: § 14.2 

The other force acting on an aircraft during flight is its weight, which is a body force and not an aerodynamic force.

See also[edit]

References[edit]

  1. ^ a b c Clancy, L.J. (1978). Aerodynamics. New York: Wiley. ISBN 0-273-01120-0. OCLC 16420565.
  • ^ Massey, B. S. (Bernard Stanford) (1998). "10.8.2". Mechanics of fluids. Vol. 2. Ward-Smith, A. J. (Alfred John) (7th ed.). Cheltenham, England: S. Thornes. ISBN 0-7487-4043-0. OCLC 40928151.
  • ^ a b c Hurt, H.H. Jr. (1965). Aerodynamics for Naval Aviators NAVAIR 00-80T-80 (PDF). U.S. Navy. pp. 14, 29, 151.
  • ^ Anderson, John D. Jr. (1999). "2.2". Aircraft performance and design. Boston: WCB/McGraw-Hill. ISBN 0-07-001971-1. OCLC 40076736.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Aerodynamic_force&oldid=1223288941"

    Category: 
    Aerodynamics
    Hidden categories: 
    Articles with short description
    Short description with empty Wikidata description
     



    This page was last edited on 11 May 2024, at 03:01 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki