Aerodynamic methods for high incidence missile design
Author:
Affiliation:
1. Martin Marietta Aerospace, Orlando, Fla.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27824
Reference11 articles.
1. Jorgensen, L. E. "A Method for Estimating Static Kerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0° to 90°, TND-7228, April 1973, NASA.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A new method for calculating wing alone aerodynamics to angle of attack 180 degrees;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
2. Calculation of wing-alone aerodynamics to high angles of attack;Journal of Spacecraft and Rockets;1995-01
3. Nonlinearities in missile aerodynamics;16th Aerospace Sciences Meeting;1978-01-16
4. Stability coefficients of a missile at angles of attack;Journal of Spacecraft and Rockets;1976-05
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