Calculation of Unsteady Subsonic Flow about Harmonically Oscillating Wing/Body Configurations
Author:
Affiliation:
1. National Aerospace Laboratory NLR, Amsterdam, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58801
Reference13 articles.
1. 2Kalman, T.P., Rodden, W.P., and Giesing, J.P. "Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow," urnalofAircraft, Vol. 8,June 1971, pp.406-413.
2. Subsonic Steady and Oscillatory Aerodynamics for Multiple Interfering Wings and Bodies
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