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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
Language: en
Pages: 36

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

Authors: Harry W. Carlson
Categories: Aerodynamics
Type: BOOK - Published: 1955 - Publisher:

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Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of
Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63
Language: en
Pages: 40

Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63

Authors: Dennis E. Fuller
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1963 - Publisher:

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Effect of Cross-section Shape on the Aerodynamic Characteristics of Bodies at Mach Numbers from 2.50 to 4.63
Language: en
Pages:

Effect of Cross-section Shape on the Aerodynamic Characteristics of Bodies at Mach Numbers from 2.50 to 4.63

Authors: Dennis E. Fuller
Categories:
Type: BOOK - Published: 1963 - Publisher:

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Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Language: en
Pages: 88

Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0

Authors: Leland Howard Jorgensen
Categories: Aerodynamics
Type: BOOK - Published: 1975 - Publisher:

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An experimental investigation was conducted in the Ames 6- by 6-Foot Wind Tunnel to measure the static aerodynamic characteristics for two bodies of elliptic cr
Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Language: en
Pages: 132

Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0

Authors: Leland Howard Jorgensen
Categories: Aerodynamics
Type: BOOK - Published: 1976 - Publisher:

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