Maximum vortex-induced side forces on slender bodies
- 8 August 1977
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Aerodynamic Characteristics of an Axisymmetric Body Undergoing a Uniform Pitching MotionJournal of Spacecraft and Rockets, 1976
- Asymmetric Vortex Effects on Missile ConfigurationsJournal of Spacecraft and Rockets, 1975
- High Angle-of-Attack Aerodynamics on a Slender Body with a Jet PlumeJournal of Spacecraft and Rockets, 1975
- Occurrence and Inhibition of Large Yawing Moments during High-Incidence Flight of Slender Missile ConfigurationsJournal of Spacecraft and Rockets, 1973
- Boundary-Layer Separation on Slender Cones at Angle of AttackAIAA Journal, 1972
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- An experimental investigation of the oscillating lift and drag of a circular cylinder shedding turbulent vorticesJournal of Fluid Mechanics, 1961
- Fluctuating Lift and Drag Acting on a Cylinder in a Flow at Supercritical Reynolds NumbersJournal of the Aerospace Sciences, 1960