Wind Tunnel Investigation Of Sonic Boom Characteristics Of A Delta Wing Body Combination At Mach Numbers Of 141 And 201 PDF Download

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An Investigation of the Influence of Lift on Sonic-boom Intensity by Means of Wind-tunnel Measurements of the Pressure Fields of Several Wing-body Combinations at a Mach Number of 2.01

An Investigation of the Influence of Lift on Sonic-boom Intensity by Means of Wind-tunnel Measurements of the Pressure Fields of Several Wing-body Combinations at a Mach Number of 2.01
Author: Harry W. Carlson
Publisher:
Total Pages: 44
Release: 1961
Genre: Aerodynamic load
ISBN:

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