论文信息 - Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation

Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation

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William J. Monta

[1] Robert W. Walters,et al. Analysis of generic scramjet external nozzle flowfields employing simulant gases , 1990 .

[2] Raymond S. Colladay. Rekindled vision of hypersonic travel , 1987 .

[3] D. P. Hearth,et al. Hypersonic technology-approach to an expanded program , 1976 .

[4] J. W. Keyes,et al. Force testing manual for the Langley 20-inch Mach 6 tunnel , 1977 .

[5] W. J. Small,et al. Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane , 1974 .

[6] J. C. Ellison,et al. REAL-GAS EFFECTS ON HYPERSONIC NOZZLE CONTOURS WITH A METHOD OF CALCULATION , 1963 .

[7] W. J. Monta,et al. A parametric experimental investigation of a scramjet nozzle at Mach 6 with Freon and argon or air used for exhaust simulation , 1991 .

[8] J. Leng,et al. Validation of scramjet exhaust simulation technique at Mach 6 , 1979 .

[9] J. P. Weidner,et al. Studies of Engine-Airframe Integration on Hypersonic Aircraft , 1971 .