Static Longitudinal Aerodynamic Characteristics At A Mach Number Of 1003 Of Low Aspect Ratio Wing Body Configurations Suitable For Reentry

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Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry

Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry
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Total Pages : 32
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ISBN-10 : NASA:31769000463631
ISBN-13 :
Rating : 4/5 ( Downloads)

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Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry Related Books

Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards
Language: en
Pages: 68
Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 to 2.86
Language: en
Pages: 126
Authors: Samuel M. Dollyhigh
Categories: Aerodynamics
Type: BOOK - Published: 1971 - Publisher:

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An experimental investigation was made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coup