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oaioai:casi.ntrs.nasa.gov:19790001849

Utilization of the wing-body aerodynamic analysis program

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1978
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Abstract

The analysis program was used to investigate several aircraft characteristics. The studies performed included vehicle stability analysis, determination of upwash angle, identification of nonpotential flow, launch dynamics, and wake vortex upset loads. The techniques and are discussed. When possible, computed results are compared with experimental data

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This paper was published in NASA Technical Reports Server.

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