- Evaluation of wind tunnel performance testing of an advanced 45 degree swept eight-bladed propeller at Mach numbers from 3-945 to 0.85
Technical Report
CID:
Authors:
Publication Date:
- 01 March 1982
Subjects:
Notes:
- (DAT) 1982
Report Number:
- NASA CR-3505
Publication Date Information:
- March 1982