Accession Number : AD0428916


Title :   COMPARISON OF HOTSHOT TUNNEL FORCE, PRESSURE HEAT-TRANSFER AND SHOCK SHAPE DATA WITH SHOCK TUNNEL DATA,


Corporate Author : ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION TENN


Personal Author(s) : Edenfield,E E


Report Date : Jan 1964


Pagination or Media Count : 25


Abstract : Comparison is made of force, pressure, heattransfer, and shock shape data from tests in the AEDC-VKF hotshot tunnels and in the Cornell Aeronautical Laboratory 48 Inch Shock Tunnel. Several cone models of varying bluntness were tested through an angle-of-attack range of 0 to 40 deg at each facility. Excellent agreement of the hotshot and the shock tunnel data is shown. (Author)


Descriptors :   *SHOCK TUBES , *CONICAL BODIES , *HYPERSONIC WIND TUNNELS , AERODYNAMICS , BLUNT BODIES , WIND TUNNEL MODELS , MODEL TESTS , PRESSURE , HEAT TRANSFER , SHOCK WAVES , SLENDER BODIES , TEST EQUIPMENT , PITCH(MOTION) , MOMENTS , LIFT , DRAG , EXPERIMENTAL DATA , ENTHALPY , EXPERIMENTAL DATA


Distribution Statement : APPROVED FOR PUBLIC RELEASE