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Combustion of Aluminum Borohydride in a Supersonic Wind Tunnel
Edward A. Fletcher
Robert G. Dorsch
Melvin Gerstein
出版
National Advisory Committee for Aeronautics
, 1955
URL
http://books.google.com.hk/books?id=xtfrjZK5Id4C&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
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.
