Errors of 7 static-pressure probes mounted very close to nose of body of revolution were determined at Mach numbers from 0.80 to 1.08 and at angles of attack from -1.7° to 8.4°; 3 of probes were equipped with gimbal system and 4 vanes that aligned probe with local flow.
Wind-tunnel tests of seven static-pressure probes at transonic speeds
NASA -- Tech Notes
1961
30 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Transonic wind-tunnel tests of error-compensated static-pressure probe
Engineering Index Backfile | 1961
|