Sting effects as determined by the measurement of pitch-damping derivatives and base pressures at Mach number 3
- 19 April 1978
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Experimental Dynamic Stability Characteristicsof a Shuttle Orbiter at M. = 8Journal of Spacecraft and Rockets, 1976
- The Effect of Sting Diameter and Length on Base Pressure at M = 3·88Aeronautical Quarterly, 1968
- Base pressure results at M equals 4 using free-flight and sting-supported models.AIAA Journal, 1968
- Radial base-pressure gradients in laminar flow.AIAA Journal, 1967
- A SPLITTER PLATE FOR THE PREVENTION OF VORTEX SHEDDING BEHIND FINITE CIRCULAR CYLINDERS IN UNIFORM CROSS FLOWPublished by Defense Technical Information Center (DTIC) ,1967
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952