Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 276

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 276

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Side Forces on Forebodies at High Angles of Attack and Mach Numbers from 0.1 to 0.7

Side Forces on Forebodies at High Angles of Attack and Mach Numbers from 0.1 to 0.7 PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 148

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 762

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Side Forces on a Tangent Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7

Side Forces on a Tangent Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7 PDF Author:
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 120

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 856

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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

AGARD Conference Proceedings

AGARD Conference Proceedings PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1040

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AIAA 22nd Fluid Dynamics, Plasma Dynamics & Lasers Conference: 91-1782 - 91-1825

AIAA 22nd Fluid Dynamics, Plasma Dynamics & Lasers Conference: 91-1782 - 91-1825 PDF Author:
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ISBN:
Category : Fluid dynamics
Languages : en
Pages : 516

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A Collection of Technical Papers

A Collection of Technical Papers PDF Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 472

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Side Forces on a Tangent Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7

Side Forces on a Tangent Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 109

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The 1979 Ames Research Center Publications: A Continuing Bibliography

The 1979 Ames Research Center Publications: A Continuing Bibliography PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 334

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