Investigation Of Aerodynamic Effects Of External Combustion Below Flat Plate Model In 10 By 10 Foot Wind Tunnel At Mach 24
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Index of NASA Technical Publications
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Index of NACA Technical Publications
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Index to NASA Technical Publications
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 300 |
Release | : 1960 |
Genre | : |
ISBN | : |
Exploratory Investigation of Aerodynamic Effects of External Combustion of Aluminum Borohydride in Airstream Adjacent to Flat Plate in Mach 2.46 Tunnel
Author | : Robert G. Dorsch |
Publisher | : |
Total Pages | : 91 |
Release | : 1957 |
Genre | : Aluminum borohydride |
ISBN | : |
Pressure distributions associated with stable combustion of aluminum borohydride in the supersonic stream adjacent to a short, 13-inch chord, and an extended, 25-inch chord, flat-plate model were determined experimentally. The models were mounted in the center of the test section of a 1- by 1-foot Mach 2.46 wind tunnel. High-speed direct and schlieren motion pictures of the flame and associated shock waves were taken, and selected photographs are presented.
Monthly Catalog of United States Government Publications
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1812 |
Release | : 1960 |
Genre | : Government publications |
ISBN | : |