The Pressure Distribution Over a Semicircular Wing Tip on a Biplane in Flight PDF Download
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Author: Richard V. Rhode Publisher: ISBN: Category : Aerodynamic load Languages : en Pages : 40
Book Description
This note presents the results of flight pressure distribution tests on the right upper wing panel of a Douglas M-3 airplane equipped with a semicircular wing tip. The results are given in tables and curves in such form that the load distribution for any normal force coefficient within the usual range encountered in flight may easily be determined.
Author: Richard V. Rhode Publisher: ISBN: Category : Aerodynamic load Languages : en Pages : 40
Book Description
This note presents the results of flight pressure distribution tests on the right upper wing panel of a Douglas M-3 airplane equipped with a semicircular wing tip. The results are given in tables and curves in such form that the load distribution for any normal force coefficient within the usual range encountered in flight may easily be determined.
Author: John Stack Publisher: ISBN: Category : Aerofoils Languages : en Pages : 556
Book Description
The effects of scale and turbulence on the lift and drag of five airfoils, the N.A.C.A. 0006 , the N.A.C.A. 0021, the Clark Y, The U.S.A 35-A, and the U.S.N. P.S.6, hve been investigated in the Variable Density Wind Tunnel. Tests were made over a wide scale for only two different conditions of turbulence.
Author: Richard V. Rhode
Author: Richard V. Rhode
Author: United States. National Advisory Committee for Aeronautics
Author: Fred E. Weick
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: 
Author: 
Author: John Stack
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics