Sideslip effects on fin-fin interference in supersonic missile aerodynamics
Author:
Affiliation:
1. McDonnell Douglas Astronautics Company, St. Louis, Missouri
2. University of Missouri—Rolla, Rolla, Missouri
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26017
Reference18 articles.
1. Supersonic flow over a cruciform configuration at angle of attack
2. A Godunov method for supersonic tactical missiles
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