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

Experimental Low-speed and Calculated High-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 65 ̊swept Delta Wing PDF Author: Jim A. Penland
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Category : Airplanes
Languages : en
Pages : 84

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NASA Technical Note

NASA Technical Note PDF Author:
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Category :
Languages : en
Pages : 572

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 704

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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Category : Government publications
Languages : en
Pages : 2834

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
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Category : United States
Languages : en
Pages : 1408

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

Low-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Delta Wing PDF Author:
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Category :
Languages : en
Pages : 82

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

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86 PDF Author: Jim A. Penland
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 88

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Compendium of NASA Langley Reports on Hypersonic Aerodynamics

Compendium of NASA Langley Reports on Hypersonic Aerodynamics PDF Author: Frances E. Sabo
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 182

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Applied mechanics reviews

Applied mechanics reviews PDF Author:
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Category : Mechanics, Applied
Languages : en
Pages : 400

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Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 PDF Author: Jim A. Penland
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Category : Aerodynamics
Languages : en
Pages : 150

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