High Reynolds number tests of a C-141A aircraft semispan model to investigate shock-induced separation
NASA contractor report ; CR-2604
1975
57 S, [67] Bl
graph. Darst
Contract no. NAS-2-8269
Report
Englisch
Structural Loads Data from C-141A Aircraft
NTIS | 1967
|C-141A Pitot-Static System Calibration Tests
NTIS | 1976
|