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:
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100 1 |a Frassinelli, Mark C. 
245 1 0 |a Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles/  |c Mark C. Frassinelli, George T. Carson, Jr 
260 |a Washington:  |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,  |c 1990 
300 |a 56 σ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA technical paper  |v 3036 
504 |a Βιβλιογραφία: σ. 11 
650 0 |a Airplanes  |x Tail surfaces 
650 0 |a Stability of airplanes, Longitudinal 
650 0 |a Aerodynamics, Transonic 
650 0 |a Jet nozzles 
700 1 |a Carson, George T. 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Division 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Division 
710 2 |a Langley Research Center 
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