Similarity Rule for Sidewall Boundary Layer Effect in Two-Dimensional Wind Tunnels
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/10.2514/3.50864
Reference11 articles.
1. Vooren, J.V.D., Sloof, J. W., Huizing, G. H., and Essen, A. V. "Remarks on the Suitability of Various Transonic Small Perturbation Equations to Describe Three-Dimensional Transonic Flow: Examples of Computations Using a Fully Conservative Rotated Difference Scheme," edited by K. Oswatitsch and D. Rues,Symposium Transsonicum II, Springer-Verlag, New York,1975, pp.557-566.
2. 2Couston, P. M. and Angelini, J. J. "Solution of Nonsteady Two-Dimensional Transonic Small Disturbance Potential Flow Equations," ONERATP 1978-69.
3. A Self-Consistent Formulation of the Transonic Small-Disturbance Theory
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