Supersonic Lift and Pitching Moment of Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration PDF Download
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Author: Frank S. Malvestuto Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 52
Book Description
Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Author: Frank S. Malvestuto Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 52
Book Description
Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Author: Publisher: ISBN: Category : Languages : en Pages : 47
Book Description
Theoretical approximations to the nondimensional lift and pitching moment produced by constant vertical acceleration, the CL(alpha) and CM(alpha) derivatives, respectively, are derived for a series of thin sweptback tapered wings with streamwise tips. The analysis is essentially the application of a recently published solution of the linearized time-dependent wave equation for wings in accelerated motion. The results are independent of camber and thickness and are applicable for a range of supersonic speed for which the wing is wholly contained between the Mach cones springing from the wing apex and from the trailing edge of the root section (subsonic leading edge and supersonic trailing edge). Design curves are presented which permit rapid estimation of the derivatives CL(alpha) and CM(alpha) for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Author: Frank S. Malvestuto Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 44
Book Description
Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Author: Isabella J. Cole Publisher: ISBN: Category : Airplanes Languages : en Pages : 67
Book Description
On the basis of a solution to the linearized time-dependent wave equation, the nondimensional lift derivative and corresponding pitching-moment derivative resulting from constant vertical acceleration (that is, linear variation of angle of attack with time) are evaluated for a family of thin sweptback tapered wings with streamwise tips traveling at supersonic speeds.
Author: Frank S. Malvestuto
Author: Frank S. Malvestuto
Author: 
Author: Frank S. Malvestuto
Author: Isabella J. Cole
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: 
Author: 
Author: Leroy Devan