1 |
Dailey, C. L., "Supersonic diffuser instability," CIT PhD Thesis, 1954.
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2 |
Mirels, H., "Acoustic analysis of ramjet buzz," NACA TN 3574, November, 1955.
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3 |
George B. Brajnikoff and arthur W. rogers, "Characteristics of four nose inlets as measured at Mach number between 1.4 and 2.0," NACA RM A51C12, June. 1951.
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4 |
Connors, J. F., and Meyers, R.C., "Design criteria for axisymmetric and two-dimensional supersonic inlets and exit," NACA TN-3589, jan. 1956.
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5 |
Fisher, S.A., Neale, M.C. and Brooks, A.J., "On the subcritical stability of variable ramp Intakes at Mach numbers around 2," NGTE Report R3111, 1970.
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6 |
John L. Allen, "Preliminary investigation of effect of performance of dividing conical-spike inlets into halves at Mach number 1.5 to 2.0," NACA RM E55I26, December 19, 1955.
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7 |
Ferri, A and Nucci, L., "The origin of aerodynamic instability of supersonic inlets at subcritical conditions," NACA RM L50K30, 1951.
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8 |
Sterbentz, W.H and Evvard, J.C., "Criterions for prediction and control of ram-jet flow pulsation," NACA TN 3506, Aug. 1955.
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9 |
Oswatitsch, K. L., "Pressure recovery for missiles with reaction propulsion at high supersonic speed (The Efficiency of shock diffuser)," NACA TM 1140, June. 1947.
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10 |
Seddon, J. and Goldsmith, E. L., "Intake aerodynamics," AIAA Education Series, 1989.
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11 |
T. J. Nussdorfer., "Some Observation of Shock-Induced Turbulent Separation on Supersonic Diffusers, "NACA RM E51L26, May. 1954.
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12 |
Gerald W. Englert and Leonard J. Obery, "Evaluation of five conical center-body supersonic diffusers at several angle of attack," NACA RM E51L04, May. 1952.
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13 |
Andrew Beke and J. L. Allen, "Forced and pressure-recovery characteristics of a conical-type nose inlet operating at Mach number of 1.6 to 2.0 and at an gles of attack to ," NACA RM E52I30, November, 1952.
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14 |
John, J. Mahoney, "Inlet for supersonic missiles," AIAA Education Series, 1990.
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15 |
lone D.V., Handbook of supersonic aerodynamics, "Duct, Nozzles and diffusers," jan, NAVWEPS Report 1488, vol. Sec.17, 1964.
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16 |
Trimpi, R. L., "An analysis of buzzing in supersonic ram jet by a modified onedimensional non-stationary wave theory," NACA TN 3695, 1956.
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17 |
Fred T. Esenwein and Alfred S. Valerino, "Force and pressure characteristics for a series of nose inlets at Mach number from 1.59 to 1.99; I -conical spike all-external compression inlet with subsonic cowl lip," NACA RM E50J26, jan. 1951.
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