Abstract
References ill, J. A. F., Wardlaw, A. B., Jr., Pronchick, S. W., and Holmes, J. E., Verification Tests in the 14 Nozzle of the Tunnel at NSWC (White Oak), AIAA Paper 77-150, Jan. 1977. Kavetsky, R., Mach 10 High Reynolds Number Development in the NSWC Facility, Naval Surface Warfare Center, TR 83-526, White Oak, MD, June 1984. Hedlund, E. R., and Ragsdale, W. C., Improvements in Low Reynolds Number Testing in the NSWC Wind Tunnel #9, AIAA Paper 85-0226, Jan. 1985. Ragsdale, W. C., Hypervelocity Wind Tunnel 9 Test Planning Guide, 2nd ed., Naval Surface Warfare Center, MP 88-200, White Oak, MD, Oct. 1989. Hedlund, E. R., Higgins, C. W., Rozanski, C. S., Fehring, N. P., and Krueger, D., The New High Reynolds Number 8 Capability in the NSWC Wind Tunnel #9, AIAA Paper 90-1379, June 1990. Trolier, J. W., Sinha, N., and York, B., Mach 8 Nozzle Design Verification, Science Applications International Corp., SAIC-88/ 1788, Fort Washington, PA, July 1988. Anon., Report 1135: Equations, Tables, and Charts for Compressible Flow, NASA Ames Research Center, Moffett Field, CA, 1953. Hecht, A. M., Nestler, D. E., and Richbourg, D. H., Application of a Three-Dimensional Viscous Computer Code to Reentry Vehicle Design, AIAA Paper 79-0306, Jan. 1979. Van Driest, E. R., The Problem of Aerodynamic Heating, Aeronautical Engineering Review, Vol. 15, No. 10, Oct. 1956, pp. 26-41.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
