Computation of Roll Moment for Projectile with Wraparound Fins Using Euler Equation
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3432
Reference12 articles.
1. Subsonic Stability and Control Characteristics of ConfigurationsIncorporating Wrap-Around Surfaces
2. Subsonic and transonic aerodynamics of a wraparound fin configuration
3. Aerodynamics of wraparound fins
4. Multiple-zone strategy for supersonic missiles
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