Summary of Propulsive-Lift Research in the Langley 16-Ft Transonic Tunnel
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58714
Reference16 articles.
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1. Application of a new adaptive grid for aerodynamic analysis of shockcontaining single jets;26th Joint Propulsion Conference;1990-07-16
2. Three-dimensional calculations for underexpanded and overexpanded supersonic jet flows;7th Applied Aerodynamics Conference;1989-07-31
3. The application of 3D marching scheme for the prediction of supersonic free jets;25th Joint Propulsion Conference;1989-07-12
4. Multiaxis aircraft control power from thrust vectoring at high angles of attack;4th Applied Aerodynamics Conference;1986-06-09
5. A static investigation of yaw vectoring concepts on two-dimensional convergent-divergent nozzles;19th Joint Propulsion Conference;1983-06-27
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