The load distribution, forces, and moments are calculated theoretically for inclined slender wing-body combinations consisting of a slender body of revolution and either a plane or cruciform arrangement of low-aspect-ratio pointed wings. The results are applicable at subsonic and transonic speeds, and at supersonic speeds, provided the entire wing-body combination lies near the center of the Mach cone.
The Aerodynamic Forces on Slender Plane- and Cruciform-Wing and Body Combinations
01.01.1950
Sonstige
Keine Angabe
Englisch
Aerodynamic forces on slender plane- and cruciform-wing and body combinations
Engineering Index Backfile | 1950
|Aerodynamic interference of slender wing-tail combinations
Engineering Index Backfile | 1957
|Aerodynamic interference of slender wing-tail combinations
TIBKAT | 1957
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