Pressure Distributions Over the Forward Portion of the Project Fire Space-vehicle Configuration at Mach Numbers from 0.25 to 0.60 PDF Download

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Pressure Distributions Over the Forward Portion of the Project Fire Space-vehicle Configuration at Mach Numbers from 0.25 to 0.60

Pressure Distributions Over the Forward Portion of the Project Fire Space-vehicle Configuration at Mach Numbers from 0.25 to 0.60 PDF Author: William P. Henderson
Publisher:
ISBN:
Category : Pressure
Languages : en
Pages : 40

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Pressure Distributions Over the Forward Portion of the Project Fire Space-vehicle Configuration at Mach Numbers from 0.25 to 0.60

Pressure Distributions Over the Forward Portion of the Project Fire Space-vehicle Configuration at Mach Numbers from 0.25 to 0.60 PDF Author: William P. Henderson
Publisher:
ISBN:
Category : Pressure
Languages : en
Pages : 40

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
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Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports PDF Author:
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ISBN:
Category : Government publications
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Keywords Index to U.S. Government Technical Reports (permuted Title Index).

Keywords Index to U.S. Government Technical Reports (permuted Title Index). PDF Author: United States. Department of Commerce. Office of Technical Services
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Category : Government publications
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Surface Pressure Distributions on 0.0628-scale Models of Proposed Project Fire Space Vehicles at Mach Numbers from 0.25 to 4.63

Surface Pressure Distributions on 0.0628-scale Models of Proposed Project Fire Space Vehicles at Mach Numbers from 0.25 to 4.63 PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
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Category : Aeronautics
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Category : Aeronautics
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Aerodynamic Load Distributions for the Project Fire Configurations at Mach Numbers from 0.25 to 4.63

Aerodynamic Load Distributions for the Project Fire Configurations at Mach Numbers from 0.25 to 4.63 PDF Author: Ralph J. Muraca
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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Heat-transfer and Pressure Distributions at Mach Numbers of 6.0 and 9.6 Over Two Reentry Configurations for the Five-stage Scout Vehicle

Heat-transfer and Pressure Distributions at Mach Numbers of 6.0 and 9.6 Over Two Reentry Configurations for the Five-stage Scout Vehicle PDF Author: Paul F. Holloway
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Category : Aerothermodynamics
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