Wind tunnel testing of helicopter rotor operating at extreme thrust coefficients and high-tip-speed ratios
RESULTS OF WIND-TUNNEL MEASUREMENTS ON A HELICOPTER ROTOR OPERATING AT EXTREME THRUST COEFFICIENTS AND HIGH-TIP-SPEED RATIOS
1963-01-01
Sonstige
Keine Angabe
Englisch
Static-thrust measurements of aerodynamic loading on helicopter rotor blade
Engineering Index Backfile | 1956
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