A Closed-form Trim Solution Yielding Minimum Trim Drag for Airplanes with Multiple Longitudinal-control Effectors

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National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989 - Drag (Aerodynamics) - 24 pages
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Contents

LOTS for TwoLiftingSurface ThrustVectoring Airplane
11
Appendix ASurface Deflections
18
References
24

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