Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers PDF Download

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Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers

Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers PDF Author: Alvin Seiff
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers

Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers PDF Author: Alvin Seiff
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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Category :
Languages : en
Pages :

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
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Category : Technology
Languages : en
Pages : 1116

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NASA Technical Note

NASA Technical Note PDF Author:
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Category :
Languages : en
Pages : 868

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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Category : Aeronautics
Languages : en
Pages : 450

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Index of N A S A Technical Publications

Index of N A S A Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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ISBN:
Category :
Languages : en
Pages : 448

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Free-flight Tests of Fifth-stage Scout Entry Vehicle at Mach Numbers of 5 and 17

Free-flight Tests of Fifth-stage Scout Entry Vehicle at Mach Numbers of 5 and 17 PDF Author: Donn B. Kirk
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Category : Space vehicles
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Transition of the Laminar Boundary Layer on a Delta Wing with 74 Degree Sweep in Free Flight at Mach Numbers from 2.8 to 5.3

Transition of the Laminar Boundary Layer on a Delta Wing with 74 Degree Sweep in Free Flight at Mach Numbers from 2.8 to 5.3 PDF Author: Gary T. Chapman
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Category : Fluid mechanics
Languages : en
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Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium

Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium PDF Author: Joseph W. Cleary
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Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 52

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A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies

A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies PDF Author: Gerald N. Malcolm
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Category : Aerodynamic characteristics
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Pages : 40

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