Methods for the Design and Analysis of Jet-Flapped Airfoils
Author:
Affiliation:
1. Douglas Aircraft Company, Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60384
Reference13 articles.
1. The lift coefficient of a thin, jet-flapped wing
2. A jet-wing lifting-surface theory using elementary vortex distributions
3. Progress in Aeronautical Science Series;Hess J. L.,1966
4. 5Stevens, W. A., Goradia, S. H., and Braden, J. A. "Mathematical Model for Two-Dimensional Multi-Component Airfoils in Viscous Flow," CR-1843,1971, NASA.
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1. Vortex developments over steady and accelerated airfoils incorporating a trailing edge jet;23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference;1993-07-06
2. A three-dimensional solution of flows over arbitrary jet-flapped configurations using a higher-order panel method;Applied Aerodynamics Conference;1983-07-13
3. Progress towards a theory of jet flap thrust recovery;21st Aerospace Sciences Meeting;1983-01-10
4. A mixed analysis and design surface panel method for two-dimensionalflows;20th Aerospace Sciences Meeting;1982-01-11
5. A quasisteady theory for incompressible flow past airfoils with oscillating jet flaps;AIAA Journal;1978-03
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