Tunnel being constructed for Air Force, to explore performance of complete propulsion systems under high altitude and speed flight conditions, including ram jet and turbojet as installed in aircraft or missiles, and for aerodynamic testing of airframes or missile models; facility will permit testing for Mach number of 0.8 to 3.5.
Propulsion wind tunnel of Arnold engineering development center at Tullahoma, Tennessee
Am Soc Mech Engrs -- Paper
American Society of Mechanical Engineers -- Meeting SA-32 ; 1953
1953
10 pages
Aufsatz (Konferenz)
Englisch
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British Library Conference Proceedings | 1998
|Arnold engineering development center
Engineering Index Backfile | 1957
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