Experimental Wake Flow Properties of a Viking '75 Entry Vehicle
- 1 January 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (1) , 11-15
- https://doi.org/10.2514/3.61997
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Aerodynamic Characteristics of Disk-Gap-Band Parachutes in the Wake of Viking Entry Forebodies at Mach Numbers from 0.2 to 2.6Published by Defense Technical Information Center (DTIC) ,1972
- Model Support Effects on Aerodynamic and Wake Characteristics of Large Angle ConesJournal of Aircraft, 1972
- Theoretical Drag Prediction for Trailing Decelerators at Supersonic SpeedsJournal of Aircraft, 1971
- Loads on bodies in wakes.Journal of Spacecraft and Rockets, 1967
- Measurements of the turbulent near wake of a cone at Mach 6.AIAA Journal, 1966
- On the velocity and temperature distributions in the turbulent wake behind a heated body of revolutionMathematical Proceedings of the Cambridge Philosophical Society, 1938