A small scale experiment for investigating the stability of a supersonic inlet

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Hongprapas, Sorarat ^a   Kozak, Jeffrey D ^a   Moses, Brooks ^a   Ng, W F ^a  

^a Virginia Polytechnic Institute and State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; CONES; REYNOLDS NUMBER;

FREESTREAM MACH NUMBER; INTERNAL FLOW PATTERNS; INTERNAL SURFACES; ONSET OF INSTABILITIES; SMALL-SCALE EXPERIMENT; STATIC MEASUREMENTS; STATIC PRESSURE MEASUREMENTS; SUPERSONIC INLETS;

INTAKE SYSTEMS;

EID: 84983134079     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Surber, L.E., and Numbers K.E., "Tactical Fighter Inlets", Intake Aerodynamics Vol. I. Von Karmen Institute of Fluid Dynamics Lecture Series 1988-04, 1988.
2. Mahoney, J.J., Inlets for Supersonic Missiles, AIAA Education Series, AIAA, Washington D.C., 1990.
3. Seddon, J. and Goldsmith, E.L., Intake Aerodynamics, AIAA Education Series, AIAA, New York, 1985.
4. Hermann, R., Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics, Minneapolis-Honeywell Regulator Co., Minneapolis, 1956.
5. Ferri, A. and Nucci, L., "The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions, " NACA RM L 50K30, 1951.
6. Sterbentz, W.H. and Evvard, J.C., "Criterion for Prediction and Control of Ramjet Flow Pulsations," NACA TN 3506, August 1955.
7. Trimpi, R.L., "An Analysis of Buzzing in Supersonic Ramjets by a Modified One-dimensional Non-stationary Wave Theory," NACA TN 3695, 1956.
8. Connors, J.F., and Wollett, R.R., "Performance Characteristics of Several Types of Axially Symmetric Nose Inlets at Mach Number 3.85," NACA RM E52I15, November 1952.
9. Nagashima, T.,Obokata, T., and Asanuma, T., "Experiment of Supersonic Intake Buzz," ISAS Report № 481, University of Tokyo, May 1972.
10. Dailey, C.L., "Supersonic Diffusers Instability," Journal of the Aeronautical Sciences, Vol. 22, № 11, November 1955, pp 733-749.
11. Maltby, R.L., and Keating, R.F.A., "The Surface Oil Flow Technique for Use in Low Speed Wind Tunnels," Flow Visualization in Wind Tunnels using Indicators, AGARDGraph #70, compiled by R.L. Maltby, 1962.
12. Hongprapas, S., "Preliminary Experiment and Analysis of Supersonic Inlet Buzz" M.S. Thesis, Virginia Tech, Blacksburg, VA, 1996.