Computer program computes zero lift wave drag of an entire aircraft including any combination of the wing, body, pods, fins, and carnard. The program computes the external volume of the wing and the axial area distribution of the wing equivalent body.
Program computes zero lift wave drag of entire aircraft
01.12.1967
Sonstige
Keine Angabe
Englisch
Zero-Lift Wave Drag of Complex Aircraft Configurations
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