Method described by J.R. SPREITER (NACA -- Report 962 indexed in Engineering Index 1951 p 743) is extended.
Pitching-moment derivatives Cmq and Cma at supersonic speeds for slender-Delta-wing and slender-body combination and approximate solutions for broad-Delta-wing and slender-body combinations
NACA -- Tech Note
1951
29 pages
Diagrs, Charts
Aufsatz (Zeitschrift)
Englisch
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