Driving mechanisms of high-speed unsteady spiked body flows, Part 1: Pulsation mode

AIAA Journal

Volumn 42, Issue 1, 2004, Pages 95-106

  Feszty, Daniel ^a   Badcock, Ken J ^a   Richards, Bryan E ^a  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FINITE VOLUME METHOD; LAMINAR FLOW; MATHEMATICAL MODELS; NUMERICAL METHODS; REYNOLDS NUMBER; SUPERSONIC FLOW;

AXISYMMETRIC FLOW; MACH NUMBER; STROUHAL NUMBER;

UNSTEADY FLOW;

EID: 0842290650     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.9034     Document Type: Article

References (30)

1. Oswatitsch, K., "Der Druckrückgewinn bei Geschossen mit Rückstossantrieb bei Hohen Überschallgeschwindigkeiten," Bericht Nr 1005, Forch. & Entwickl. Heereswaffenamtes and NACA TM 1140, 1944.
2. Lu, P., and Jain, L., "Numerical Investigation of Inlet Buzz," Journal of Propulsion and Power, Vol. 14, No. 1, 1998, pp. 90-99.
3. Mair, W., "Experiments on Separation of Boundary Layer on Probes in Front of Blunt Nosed Bodies in a Supersonic Stream," Philosophical Magazine, Vol. 43, No. 342, July 1952, p. 593-601.
4. Bogdonoff, S., and Vas, I., "Preliminary Investigations of Spiked Bodies at Hypersonic Speeds," Journal of the Aerospace Sciences, Vol. 26, No. 2, 1959, pp. 65-74.
5. Maull D. J., "Hypersonic Flow over Axially Symmetric Spiked Bodies," Journal of Fluid Mechanics, Vol. 8, 1994, pp. 584-592.
6. Yamauchi, M., and Fujii, K., and Highashino, F., "Numerical Investigation of Supersonic Flows Around Spiked Blunt Body," Journal of Spacecraft and Rockets, Vol. 32, No. 1, 1995, pp. 32-42.
7. Ganiev, Y., Gordeev, V., Krasilnikov, A., Lagutin, V., Otmennikov, V., and Panasenko, A., "Aerodynamic Drag Reduction by Plasma and Hot-Gas Injection," Journal of Thermophysics and Heat Transfer, Vol. 14, No. 1, 2000, pp. 10-17.
8. Roberts, B., "An Experimental Study of the Drag of Rigid Models Representing Two Parachute Designs at M = 1.40 and 2.19," Royal Aircraft Establishment, TN Aero 2734, 1960.
9. Maynard, J., "Aerodynamics Characteristics of Parachutes at Mach Numbers 1.6 to 3.0," NASA TN D 752, 1961.
10. Minges, M., "Ablation Phenomenology (a Review)," High Temperatures - High Pressures, Vol. 1, No. 6, 1969, pp. 607-649.
11. Abbett, M., Cooper, L., Dahm, T., and Jackson, M., "Flow Characteristics About Concave Conic Forebodies at High Mach Numbers," AIAA Paper 75-153, 1975
12. AIAA Journal, Vol. 13, No. 11, 1975, pp. 1419, 1420.
13. Kabelitz, H., "Zur Stabilität Geschlossener Greznschichtablösegebeite an Konischen Drehkörpern bei Hyperschallströmung," DLR, FB: 71-77, Germany, 1971.
14. Wood, C. "Hypersonic Flow Over Spiked Cones," Journal of Fluid Mechanics, Vol. 12, No. 4, 1961, pp. 614-624.
15. Holden, M. "Experimental Studies of Separated Flows at Hypersonic Speeds. Part I - Separated Flows over Axisymmetric Spiked Bodies," AIAA Journal, Vol. 4, No. 4, 1966, pp. 23, 23.
16. Kenworthy, M. "A Study of Unstable Axisymmetric Separation in High Speed Flows," Ph.D Dissertion, Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 1978.
17. Antonov, A., and Gretsov, V., and Shalaev, S., "Experimental Investigation of the Characteristics of Unsteady Separated Regions Arising in the Supersonic Flow at a Spiked Body," Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, Aug. 1976, pp. 118-124.
18. Panaras, A., "Pulsating Flows About Axisymmetric Concave Bodies," AIAA Journal, Vol. 19, No. 6, 1981, pp. 804-806.
19. Zapriagaev, V., and Mironov, S., "An Experimental Study of Fluctuations in the Front Separation Zone at Supersonic Flow Velocities," Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, Aug. 1989, pp. 116-124.
20. Shang, J., and Hankey, W., "Flow Oscillations of Spike-Tipped Bodies," AIAA Journal, Vol. 20, No. 1, 1981, pp. 25, 26.
21. Ingram, C. L., McRae, D., and Benson, R., "Time-Accurate Simulation of a Self-Excited Oscillatory Supersonic External Flow with a Multi-Block Solution Adaptive Mesh Algorithm," AIAA Paper 93-3387-CP, 1993
22. Freszty, D., Badcock, K., and Richards, B., "Utilising CFD in the Investigation of High-Speed Spiked Body Flows," Aeronautical Journal, Vol. 106, No. 1058, 2002, pp. 161-174.
23. Edney, B., "Effects of Shock Impingement on the Heat Transfer Around Blunt Bodies," AIAA Journal, Vol. 6, No. 1, 1968, pp. 15-21.
24. Rockwell, D., and Naudascher, E., "Self-Sustained Oscillations of Impinging Free Shear Layers," Annual Review of Fluid Mechanics, Vol. 11, 1979, pp. 67-94.
25. Badcock, K., Richards, B., and Woodgate, M., "Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers," Progress in Aerospace Sciences, Vol. 36, 2000, pp. 351-392.
26. Gnoffo, P., "Point-Implicit Relaxation Strategies for Viscous Hypersonic Flows," Computational Methods in Hypersonic Aerodynamics, edited by T. K. S. Murthy, Kluwer Academic, Norwell, MA, 1993, pp. 115-151.
27. "Equations, Tables, and Charts for Compressible Flow," NACA 1135, 1953.
28. Ferri, A., and Nucci, L., "The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions," NACA RM L50 K30, Jan. 1951.
29. Feszty, D., Badcock, K., Richards, B., and Woodgate, M., "Numerical Simulation of a Pulsating Flow Arising over an Axisymmetric Spiked Blunt Body at Mach 2.21 and Mach 6.00," Shock Waves, Vol. 10, No. 5, 2000, pp. 323-331.
30. Feszty, D., "Numerical Simulation and Analysis of High-Speed Unsteady Spiked Body Flows," Ph.D. Dissertion, Dept. of Aerospace Engineering, Univ. of Glasgow, Glasgow, Scotland, U.K., 2001.