Asymmetric Vortex Effects on Missile Configurations
- 1 November 1975
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 12 (11) , 674-681
- https://doi.org/10.2514/3.57034
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Prediction of Yawing Force at High Angle of AttackAIAA Journal, 1974
- Approximate Method for Estimating Wake Vortex StrengthAIAA Journal, 1974
- Aerodynamic forces and moments on a slender body with a jet plume for angles of attack up to 180 degreesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971
- The Estimation of the Drag of Circular Cylinders at Subcritical Reynolds Numbers and Subsonic SpeedsThe Aeronautical Journal, 1970
- Distribution of local pressure and skin friction around a circular cylinder in cross-flow up to Re = 5 × 106Journal of Fluid Mechanics, 1968
- The Estimation of Normal-Force, Drag, and Pitching-Moment Coefficients for Blunt-Based Bodies of Revolution at Large Angles of AttackJournal of the Aeronautical Sciences, 1954