Author: Harrison Allen
Publisher:
ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20
Book Description
A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel
Author: Harrison Allen
Publisher:
ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20
Book Description
Exploratory 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
Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4
Author: Robert G. Dorsch
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 34
Book Description
NASA Technical Note
Combustion of Aluminum Borohydride in a Supersonic Wind Tunnel
Author: Edward A. Fletcher
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82
Book Description
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.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82
Book Description
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 ...
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1812
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1812
Book Description