Author: Donald S. Woolston
Publisher:
ISBN:
Category : Oscillating wings (Aerodynamics)
Languages : en
Pages : 25
Book Description
Aerodynamic forces and moments associated with flapping oscillations of finite wings at low speeds are considered. A comparison of theoretical and experimental results is made for a rectangular wing of aspect ratio 2. Calculated results are also given for three tapered wings of aspect ratio 3 with varying amounts of sweepback. The calculations are based on a numerical solution of the integral equation of subsonic lifting-surface theory. The experimental techniques employed are essentially those used in previous measurements associated with pitching oscillations. Theory and experiment are generally in good agreement with regard to magnitude of the forces and moments, but differ with regard to phase angle.
Analytical and Experimental Investigation of Aerodynamic Forces and Moments on Low-aspect-ratio Wings Undergoing Flapping Oscillations
Author: Donald S. Woolston
Publisher:
ISBN:
Category : Oscillating wings (Aerodynamics)
Languages : en
Pages : 25
Book Description
Aerodynamic forces and moments associated with flapping oscillations of finite wings at low speeds are considered. A comparison of theoretical and experimental results is made for a rectangular wing of aspect ratio 2. Calculated results are also given for three tapered wings of aspect ratio 3 with varying amounts of sweepback. The calculations are based on a numerical solution of the integral equation of subsonic lifting-surface theory. The experimental techniques employed are essentially those used in previous measurements associated with pitching oscillations. Theory and experiment are generally in good agreement with regard to magnitude of the forces and moments, but differ with regard to phase angle.
Publisher:
ISBN:
Category : Oscillating wings (Aerodynamics)
Languages : en
Pages : 25
Book Description
Aerodynamic forces and moments associated with flapping oscillations of finite wings at low speeds are considered. A comparison of theoretical and experimental results is made for a rectangular wing of aspect ratio 2. Calculated results are also given for three tapered wings of aspect ratio 3 with varying amounts of sweepback. The calculations are based on a numerical solution of the integral equation of subsonic lifting-surface theory. The experimental techniques employed are essentially those used in previous measurements associated with pitching oscillations. Theory and experiment are generally in good agreement with regard to magnitude of the forces and moments, but differ with regard to phase angle.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1160
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1160
Book Description
Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594
Book Description
NASA Technical Report
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 652
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 652
Book Description
Experimental Determination of the Pressure Distribution on a Rectangular Wing Oscillating in the First Bending Mode for Mach Numbers from 0.24 to 1.30
Author: Henry C. Lessing
Publisher:
ISBN:
Category : Aerodynamics, aircraft
Languages : en
Pages : 98
Book Description
Publisher:
ISBN:
Category : Aerodynamics, aircraft
Languages : en
Pages : 98
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 382
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 382
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1516
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1516
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.