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Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles/

Main Author:	Frassinelli, Mark C.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Other Authors:	Carson, George T.
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990
Series:	NASA technical paper 3036
Subjects:	Airplanes > Tail surfaces Stability of airplanes, Longitudinal Aerodynamics, Transonic Jet nozzles

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