Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6
Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86
Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63
Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
Book Description
The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0
Author: W. F. Lindsey
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Aerodynamic Characteristics for Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-stream Mach Numbers from 1.50 to 1.99
Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies
Author: Louis S. Stiver
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 108
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 108
Book Description
Effects of Body Shape on the Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6
Author: Walter P. Nelms
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 68
Book Description
Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept
Author: Gregory D. Riebe
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 34
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 208
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 208
Book Description