-PDF Download- Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Swept Double Delta Wing At Mach Numbers From 150 To 286 EBOOK

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86

Author: Jim A. Penland

Publisher:

Published: 1975

Total Pages: 88

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Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Number 0.2

Author: Jim A. Penland

Publisher:

Published: 1978

Total Pages: 86

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Low-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Delta Wing

Author:

Publisher:

Published: 1974

Total Pages: 82

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Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70 ̊swept delta wing

Author: Louis E. Clark

Publisher:

Published: 1977

Total Pages: 68

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Experimental Low-speed and Calculated High-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 65 ̊swept Delta Wing

Author: Jim A. Penland

Publisher:

Published: 1974

Total Pages: 84

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Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane

Author: James L. Dillon

Publisher:

Published: 1978

Total Pages: 68

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An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow

Author: Mitchel H. Bertram

Publisher:

Published: 1963

Total Pages: 136

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Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.