Supersonic Lifting-Surface Computer Program for Cruciform Wing-Body Combinations.
Technical rept. 1 Oct 73-30 Sep 74,
NIELSEN ENGINEERING AND RESEARCH INC MOUNTAIN VIEW CALIF
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A lifting-surface computer program has been written for supersonic cruciform wing-body combinations at combined pitch and yaw conditions. The method involves supersonic line sources and doublets to model the body and uses Woodwards constant pressure panels to represent the wing. Such panels are also placed on the body surface to account for wing-body interference.
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