Author: James F. CampbellPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63
Author: James F. CampbellPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63
Author: James F. CampbellLongitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers
Author: George C. AshbyPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
Book Description
Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing
Author: Edward J. RayLongitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40 Deg Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96
Author: Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing
Author: An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations
Author: Harry W. CarlsonPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.
Author: 
Author: W. P. Henderson
Author: Edwin E. Davenport