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A Flight Investigation Of The Transonic Area Rule For A 52 5 Sweptback Wind Body Configuration At Mach Numbers Between 0 8 And 1 6


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Transonic Wind-tunnel Investigation of the Effects of Aspect Ratio, Spanwise Variations in Section Thickness Ratio, and a Body Indentation on the Aerodynamic Characteristics of a 45© Sweptback Wing-body Combination


Transonic Wind-tunnel Investigation of the Effects of Aspect Ratio, Spanwise Variations in Section Thickness Ratio, and a Body Indentation on the Aerodynamic Characteristics of a 45© Sweptback Wing-body Combination

Author: Melvin M. Carmel

language: en

Publisher:

Release Date: 1953


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Index of NACA Technical Publications


Index of NACA Technical Publications

Author: United States. National Advisory Committee for Aeronautics

language: en

Publisher:

Release Date: 1957


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Transonic and Supersonic Wind-tunnel Tests of Wing-body Combinations Designed for High Efficiency at a Mach Number of 1.41


Transonic and Supersonic Wind-tunnel Tests of Wing-body Combinations Designed for High Efficiency at a Mach Number of 1.41

Author: Frederick C. Grant

language: en

Publisher:

Release Date: 1960


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