Base Flow Characteristics for Several Four-clustered Rocket Configurations at Mach Numbers from 2.0 to 3.5 PDF Download

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Base Flow Characteristics for Several Four-clustered Rocket Configurations at Mach Numbers from 2.0 to 3.5

Base Flow Characteristics for Several Four-clustered Rocket Configurations at Mach Numbers from 2.0 to 3.5 PDF Author: Normal T. Musial
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 60

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Base Flow Characteristics for Several Four-clustered Rocket Configurations at Mach Numbers from 2.0 to 3.5

Base Flow Characteristics for Several Four-clustered Rocket Configurations at Mach Numbers from 2.0 to 3.5 PDF Author: Normal T. Musial
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 60

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1990

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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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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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ISBN:
Category : Aeronautics
Languages : en
Pages : 450

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Index of NASA Technical Publications

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

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Experimental Investigation of Base Flow Field at High Altitudes for Configurations of Four and Five Clustered Nozzles

Experimental Investigation of Base Flow Field at High Altitudes for Configurations of Four and Five Clustered Nozzles PDF Author: R. A. Wasko
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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NASA SP. PDF Author:
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Category : Aeronautics
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Pages : 464

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International Aerospace Abstracts PDF Author:
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Category : Aeronautics
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Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors

Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors PDF Author: Dennis E. Fuller
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

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Aero/space Engineering

Aero/space Engineering PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 874

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