Shape sensitivity analysis of wing static aeroelastic characteristics
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Virginia Polytechnic Institute and State University, Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2301
Reference4 articles.
1. Nx= 5 N = 6 for Wings Having Arbitrary Plan Form,' NACA Y Report No. 921, 1948. Table 2. Effect of Aerodynamic Model Discretization on Convergence
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