A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel PDF Download

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A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel

A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel PDF Author: Harrison Allen
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ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20

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A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel

A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel PDF Author: Harrison Allen
Publisher:
ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20

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Exploratory Investigation of Static- and Base-pressure Increases Resulting from Combustion of Aluminum Borohydride Adjacent to Body of Revolution in Supersonic Wind Tunnel

Exploratory Investigation of Static- and Base-pressure Increases Resulting from Combustion of Aluminum Borohydride Adjacent to Body of Revolution in Supersonic Wind Tunnel PDF Author: Robert G. Dorsch
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ISBN:
Category :
Languages : en
Pages : 49

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Exploration Investigation of Static- and Base-pressure Increases Resulting from Combustion of Aluminum Borohydride Adjacent to Body of Revolution in Supersonic Wind Tunnel

Exploration Investigation of Static- and Base-pressure Increases Resulting from Combustion of Aluminum Borohydride Adjacent to Body of Revolution in Supersonic Wind Tunnel PDF Author: John S. Serafini
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Category :
Languages : en
Pages : 49

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Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4

Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4 PDF Author: Robert G. Dorsch
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ISBN:
Category : Mach number
Languages : en
Pages : 34

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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category :
Languages : en
Pages : 396

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Combustion of Aluminum Borohydride in a Supersonic Wind Tunnel

Combustion of Aluminum Borohydride in a Supersonic Wind Tunnel PDF Author: Edward A. Fletcher
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82

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The feasibility of adding heat to a supersonic airstream in the absence of flameholders was studied. Transient burning for periods of 3 to 10 milliseconds was achieved in a supersonic wind tunnel at nominal Mach numbers of 1.5, 2, 3, and 4. Steady burning was achieved for periods of 0.2 to 2 seconds at nominal Mach numbers of 1.5, 2, and 3. Burning and tunnel flow phenomena, including thermal choking, are described. Possible applications of the results of this study are suggested.

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 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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Index of NASA Technical Publications

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

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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ISBN:
Category : Government publications
Languages : en
Pages : 1812

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