Approximate Calculation of Aerodynamic Coefficients for Rotating Slender Bodies at 90 deg Incidence
- 1 January 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 19 (1) , 84-86
- https://doi.org/10.2514/3.62209
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Wind tunnel investigations for the flat spin of slender bodies at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Steady and Unsteady Vortex-Induced Asymmetric Loads on Slender VehiclesJournal of Spacecraft and Rockets, 1981
- On the Aerodynamic Force Acting on a Circular Cylinder in the Critical Range of the Reynolds NumberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- On vortex shedding from a circular cylinder in the critical Reynolds number régimeJournal of Fluid Mechanics, 1969