This report presents results of an investigation carried out in the Naval Ordnance Laboratory's Supersonic Tunnel Number 1 to determine the aerodynamic characteristics of the AGARD Calibration Model B. Tests were conducted at free-stream Mach numbers ranging from 0.70 to 3.50, at angles of attack from -4 to +10 degrees, over a Reynolds number range from 0.20 times 100to the 6th power to 0.62 times 10 to the 6th power. (Author)
Wind Tunnel Measurements of the AGARD Calibration Model B at Transonic and Supersonic Speeds
1964
24 pages
Report
Keine Angabe
Englisch
Aerodynamics , Laboratory & Test Facility Design & Operation , Wind tunnel models , Supersonic wind tunnels , Calibration , Ogines , Cylindrical bodies , Subsonic flow , Transonic flow , Supersonic flow , Heat transfer , Pressure , Lift , Pitch (Motion) , Test facilities , Measurement , Delta wings , Transonic wind tunnels
AGARD wind tunnel calibration models
Engineering Index Backfile | 1958
Wind Tunnel Blockage Effects on the AGARD B Model in Transonic Flow
British Library Online Contents | 1994
|Wind Tunnel Blockage Effects on the AGARD B Model in Transonic Flow
British Library Conference Proceedings | 1994
|Recent developments in wind-tunnel testing techniques at transonic and supersonic speeds
Engineering Index Backfile | 1964
|