Unsteady aerodynamic loads on slender cones at free-stream Mach numbers from 0 to 22
Author:
Affiliation:
1. Bolt Beranek and Newman, Inc., Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-998
Reference9 articles.
1. Houbolt. J.C. "Onthe Estimation of Pressure Fluctuations in Boundary Layers and Wakes, 'I GE-TIS - April 1966.
2. PREDICTION OF BOUNDARY LAYER PRESSURE FLUCTUATIONS
3. Ailman, C. M. "On Predicting Fluctuatlng Pressures at a Wall Beneath a Turbulent Boundary Layer, IfDouglas Paper No. 4331, April 1967.
4. Martellucci, A., Chaump, L., Rogers, D., and Smith, D. "Experimental Determinatlon of the Aero-Acoustic Environment About a Slender Cone," AIAA Paper No. 72-706,1972.
5. Conversationwith Harry Himmelblauof Rockwell International, DOC. 1972. c
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