Computer programs predict effect of slipstream-wing flow interaction on aerodynamic characteristics of deflected slipstream and tilt aircraft. One program calculates lift distribution, lift, and drag of wing in wide slipstream. Results permit development of simplified lifting surface theory for circular jet.
Lift distribution in a rectangular jet
1971-02-01
Sonstige
Keine Angabe
Englisch
Experimental lift distribution across span of stalled rectangular aerofoil
Engineering Index Backfile | 1939
|Engineering Index Backfile | 1940
|Emerald Group Publishing | 1944
|Engineering Index Backfile | 1944
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