Author: Irving Weinstein
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 40
Book Description
Heat Transfered and Pressure Distributions on a Hemisphere-cylinder and a Bluff-afterbody Model in Methane-air Combustion Products and in Air
Author: Irving Weinstein
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 40
Book Description
Exploratory Study of Open-face Honeycomb to Reduce Temperature of Hypersonic Aircraft Structure
Author: Lewis Roane Hunt
Publisher:
ISBN:
Category : Honeycomb structures
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Honeycomb structures
Languages : en
Pages : 36
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1042
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1042
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Book Description
Heat-transfer and Pressure Distributions on Hemisphere-cylinders in Methane-air Combustion Products at Mach 7
Author: Irving Weinstein
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
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.
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
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
Author: G. M. Gregorek
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 64
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1284
Book Description
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1284
Book Description
Experimental Investigation of Heat-transfer Distributions in Deep Cavities in Hypersonic Separated Flow
Author: Allan R. Wieting
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 36
Book Description
Hypervelocity wind tunnel tests to determine local cold wall convective heating rates to small rectangular cavities,
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 36
Book Description
Hypervelocity wind tunnel tests to determine local cold wall convective heating rates to small rectangular cavities,