Heat Transfered and Pressure Distributions on a Hemisphere-cylinder and a Bluff-afterbody Model in Methane-air Combustion Products and in Air

Heat Transfered and Pressure Distributions on a Hemisphere-cylinder and a Bluff-afterbody Model in Methane-air Combustion Products and in Air PDF Author: Irving Weinstein
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 40

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Exploratory Study of Open-face Honeycomb to Reduce Temperature of Hypersonic Aircraft Structure

Exploratory Study of Open-face Honeycomb to Reduce Temperature of Hypersonic Aircraft Structure PDF Author: Lewis Roane Hunt
Publisher:
ISBN:
Category : Honeycomb structures
Languages : en
Pages : 36

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1042

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 262

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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: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258

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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 620

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Heat-transfer and Pressure Distributions on Hemisphere-cylinders in Methane-air Combustion Products at Mach 7

Heat-transfer and Pressure Distributions on Hemisphere-cylinders in Methane-air Combustion Products at Mach 7 PDF Author: Irving Weinstein
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

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Book Description
Heat-transfer and pressure distributions were measured over the surfaces of three hemisphere-cylinder models tested at a nominal Mach number of 7 in the Langley 8-foot high-temperature structures tunnel which uses methane-air products of combustion as a test medium. The results showed that the heat-transfer and pressure distributions over the surface of the models were in good agreement with experimental data obtained in air and also with theoretical predictions.

A Variable Atmosphere Hypersonic Wind Tunnel for Similitude Studies

A Variable Atmosphere Hypersonic Wind Tunnel for Similitude Studies PDF Author: G. M. Gregorek
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 64

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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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ISBN:
Category : United States
Languages : en
Pages : 1284

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Experimental Investigation of Heat-transfer Distributions in Deep Cavities in Hypersonic Separated Flow

Experimental Investigation of Heat-transfer Distributions in Deep Cavities in Hypersonic Separated Flow PDF Author: Allan R. Wieting
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 36

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Hypervelocity wind tunnel tests to determine local cold wall convective heating rates to small rectangular cavities,