Body-axis rolling motion critical states of a 65-degree delta wing
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7531
2. Institute for Aerospace Research, Ottawa, Ontario K1A OR6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46933
Reference23 articles.
1. 5Truong, K. V., and Tobak, M. "Indicial Response Approach Derived from Navier-Stokes Equations: Part 1-Time-Invariant Equilibrium State," NASA TM-102856, Oct.1990.
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