Prediction of the Nonlinear Aerodynamic Characteristics of Tandem-Control and Rolling-Tail Missiles
Author:
Affiliation:
1. Nielsen Engineering and Research Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4511
Reference20 articles.
1. Analysis of selected data from the triservice missile data base
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