Recent advances in the aerothermodynamics of spiked hypersonic vehicles

Progress in Aerospace Sciences

Volumn 47, Issue 6, 2011, Pages 425-449

  Ahmed, M Y M ^a   Qin, N ^b  

^a MILITARY TECHNICAL COLLEGE   (Egypt)

^b UNIVERSITY OF SHEFFIELD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; DRAG; HYPERSONIC AERODYNAMICS; PLASMA SHOCK WAVES;

EXPERIMENTAL FACILITIES; HIGH SPEED VEHICLES; HYPERSONIC SPEED; ON BOARD EQUIPMENTS; RECIRCULATING FLOW; SIMULATION TECHNIQUE; STAGNATION POINTS; VOLUMETRIC EFFICIENCY;

HYPERSONIC VEHICLES;

EID: 80052712124     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.paerosci.2011.06.001     Document Type: Review

References (96)

1. V. Menezes, S. Saravanan, and K.P.J. Reddy Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers Shock Waves 12 1 2002 197 204 (Pubitemid 36185445)
2. Shoemaker, JM. Aerodynamic spike flowfields computed to select optimum configuration at Mach 2.5 with experimental validation. AIAA paper 90-0414; 1990.
3. White, JT. Application of NavierStokes flowfield analysis to the aerothermodynamic design of an aerospike-configured missile. AlAA paper 93-0968; 1993
4. P. Gnemmi, J. Srulijes, and K. Roussel Flowfield around spike-tipped bodies for high attack angles at Mach 4.5 Journal of Spacecraft and Rockets 40 5 2003 622 631
5. R.C. Mehta Numerical heat transfer study over spiked blunt bodies at Mach 6.8 Journal of Spacecraft and Rockets 37 5 2000 700 703
6. Heubner LD Mitchell AM, Boudreaux EJ. Experimental results on the feasibility of an aerospike for hypersonic missiles. AIAA paper, 95-0737; January 1995.
7. R.C. Mehta Peak heating for reattachment of separated flow on a spiked blunt body Heat and Mass Transfer 36 2000 277 283
8. Wagner RD, Pine CP. Laminar heat transfer and pressure distribution studies on a series on re-entry nose shapes at a Mach number of 19.4 in Helium. NASA TN D-891; 1961.
9. D.J. Maull Hypersonic flow over axially symmetric spiked bodies Journal of Fluid Mechanics 8 P.4 1960 584 592
10. V. Menezes, S. Saravanan, G. Jagadeesh, and K.P.J. Reddy Experimental investigations of hypersonic flow over highly blunted cones with aerospikes AIAA Journal 41 10 2003 1955 1966
11. S.M. Bogdonoff, and I.E. Vas Preliminary investigations of spiked bodies at hypersonic speeds Journal of the Aerospace Sciences 26 2 1959 65 74
12. Mehta RC. Flow field computations over conical, disc and flat spiked body at Mach 6. AIAA paper 2009-325; 2009.
13. Alexander SR. Results of tests to determine the effect of a conical windshield on the drag of a bluff body at supersonic speeds.NACA RM L6K08a; January 1947.
14. J.P. Reding, R.A. Guenther, and B.J. Richter Unsteady aerodynamic considerations in the design of a drag-reduction spike Journal of Spacecraft and Rockets 14 1 1977 54 60
15. M. Gauer, and A. Paull Numerical investigation of a spiked blunt nose cone at hypersonic speeds Journal of Spacecraft and Rockets 45 3 2008 459 471
16. R. Kalimuthu, R.C. Mehta, and E. Rathakrishnan Experimental investigation on spiked body in hypersonic flow The Aeronautical Journal 112 1136 2008 593 598
17. A.G. Panaras, and D. Drikakis High-speed unsteady flows around spiked-blunt bodies Journal of Fluid Mechanics 632 2009 69 96
18. W. Calarese, and W. Hankey Modes of shock-wave oscillations on spike-tipped bodies AIAA Journal 23 2 1985 185 192 (Pubitemid 15457785)
19. H.H. Album Regarding the utility of spiked blunt bodies Journal of the Aerospace Sciences 5 1 1968 112 113
20. R.A. Guenther, and J.P. Reding Fluctuating pressure environment of a drag reduction spike Journal of Spacecraft and Rockets 14 12 1977 705 710 (Pubitemid 8561288)
21. Motoyama N, Mihara K, Miyajima R, Watanuki T, Kubota H. Thermal protection and drag reduction with use of spike in hypersonic flow. AIAA paper 2001-1828; 2001
22. C.J. Wood Hypersonic flow over spiked cones Journal of Fluid Mechanics 12 Pt. 4 1961 614 624
23. Crawford DH. Investigation of the flow over a spiked-nose hemisphere-cylinder. NASA TN-D-118; December 1959.
24. Kurbatskii KA, Montanari F. Application of pressure-based coupled solver to the problem of hypersonic missiles with aerospikes. AIAA paper 2007462; 2007.
25. S.S. Milicev, and M.D. Pavlovic Influence of spike shape at supersonic flow past blunt-nosed bodies: experimental study AIAA Journal 40 5 2001 1018 1020 (Pubitemid 34599894)
26. McGhee RJ, Staylor WF. Aerodynamic investigation of sharp cone-cylinder spikes on 1200 blunted cones at Mach numbers of 3, 4.5, and 6. NASA TN D-5201; 1969.
27. A.G. Mikhail Spike-nosed projectiles: computations and dual flow modes in supersonic flight Journal of Spacecraft and Rockets 28 4 1991 418 424
28. Piland RO, Putland LW. Zero-lift drag of several conical and blunt nose shapes obtained in free flight at Mach number of 0.7 to 1.3. NACA RM L54A27; March 1954.
29. W.H. Sims, D.E. Boylan, and J.S. Hahn Drag on blunt bodies with and without spikes in low-density hypersonic flow AIAA Journal 3 2 1965 365 366
30. M. Holden Experimental studies of separated flows at hypersonic speeds. Part I - separated flows over axisymmetric spiked bodies AIAA Journal 4 4 1966 591 599
31. Z. Jiang, Y. Liu, G. Han, and W. Zhao Experimental demonstration of a new concept of drag reduction and thermal protection for hypersonic vehicles Acta Mechanica Sinica 25 3 2009 417 419
32. Guy Y, McLaughlin TE, Morrow JA. Blunt body wave reduction by means of a standoff spike. AIAA paper 2001-0888; 2001.
33. Beastall D, Turner J. The effect of a spike protruding in front of a bluff: body at supersonic speeds. Aeronautical Research Council, R. & M. No. 3007; 1957.
34. Stalder JR, Nielson HV. Heat transfer from a hemisphere cylinder equipped with flow separation spikes. NACA TN 3287, September 1954.
35. Moeckel WE. Flow separation ahead of a blunt axially symmetric body at Mach Numbers 1.76 to 2.10. NACA RM E51I25; 1951.
36. W.A. Mair Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream Philosophy Magazine, Series 7 43 243 1952 695 716
37. Jones JJ. Flow separation from rods ahead of blunt noses at Mach number 2.7. NACA RM L52E05a; July 1952.
38. Jones JJ. Experimental drag coefficients of round noses with conical windshields at Mach Number 2.72. NACA RM L55E10; June 1955.
39. Hermach CA, Kraus K, Reller JO. Reduction in temperature-recovery factor associated with pulsating flows generated by spike-nosed cylinders at a Mach number of 3.50. NACA RM A56L05; March 1957.
40. Chapman DR, Kuehn DM, Larson HK. Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition. NACA TR 1356; 1957.
41. V.S. Khlebnikov Distribution of heat flux on the surface of a sphere with a forward separation zone Fluid Dynamics 21 4 1986 654 658 (Pubitemid 17573634)
42. Staylor WF. Flow-field investigation for large-angle cones with short spikes at a Mach number of 9.6. NASA TN D-5754; 1970.
43. G. DHumieres, and J.L. Stollery Drag reduction on a spiked body at hypersonic speeds The Aeronautical Journal 114 1152 2010 113 119
44. S.S. Milicev, M.D. Pavlovic, S. Ristic, and A. Vitic On the influence of spike shape at supersonic flow past blunt bodies Mechanics, Automatic Control and Robotics 3 12 2002 371 382
45. R. Kalimuthu, R.C. Mehta, and E. Rathakrishnan Drag reduction for spike attached to blunt-nosed body at Mach 6 Journal of Spacecraft and Rockets 47 1 2010 219 222
46. V.N. Myshenkov Numerical investigation of separated flow in front of a spiked cylinder Fluid Dynamics 16 6 1981 938 942
47. V.M. Paskonov, and N.A. Cheranova Numerical investigation of laminar separation in the case of supersonic flow of viscous gas past spiked bodies Fluid Dynamics 19 2 1984 281 285 (Pubitemid 14664190)
48. V.N. Karlovskii, and V.I. Sakharov Numerical investigation of supersonic flow past blunt bodies with protruding spikes Fluid Dynamics 21 3 1986 437 445 (Pubitemid 17498016)
49. A.G. Mikhail Spike-nosed projectiles with vortex rings: steady and nonsteady flow simulations Journal of Spacecraft and Rockets 33 1 1996 8 14 (Pubitemid 126556587)
50. Hur KH, Kirn ST, Lee DH. Numerical analysis on supersonic, viscous flowfield around a spike-nosed projectile with fins. AIAA paper 96-3449-CP; 1996.
51. M. Yamauchi, K. Fujii, and F. Higashino Numerical investigation of supersonic flows around a spiked blunt body Journal of Spacecraft and Rockets 32 1 1995 32 42
52. R.C. Mehta Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6.8 Shock Waves 11 3 2002 431 440 (Pubitemid 40849808)
53. Asif M, Zahir S, Kamran N, Khan M. Computational investigations aerodynamic forces at supersonic/hypersonic flow past a blunt body with various forward facing spikes. AIAA paper 20045189; 2004.
54. Srinivasan GR, Chamberlain RR. Drag reduction of spiked missile by heat addition. AIAA paper 2004-4714; 2004.
55. J.P. Reding, and D.M. Jecmen Effects of external burning on spike-induced separated flow Journal of Spacecraft and Rockets 20 5 1983 452 453 (Pubitemid 14468256)
56. Jagadeesh G, Viren M, Reddy KPJ, Hashimoto T, Sun M, Takayama K. Hypersonic buzz phenomenon in the spiked blunt cones. AIAA paper 2003-284; 2003.
57. Srulijes J, Gnemmi P, Seiler F, Runne K. Shock tunnel high speed photography and CFD calculations on spike-tipped bodies. FrenchGerman Research Inst. of Saint-Louis, ISL Rept. PU 649/2002, Saint-Louis Codex, France; SeptemberOctober 2002.
58. Kulkarni V, Kulkarni PS, Reddy KPJ. Drag reduction by a forward facing aerospike for a large angle blunt cone in high enthalpy flows. In: Proceedings of the 26th international symposium on shock waves; July 2007. p. 56670.
59. Roveda R. Benchmark CFD study of spiked blunt body configurations. AIAA paper 2009-367; 2009.
60. Kabelitz H. Zur Stabilität Geschlossener Greznschichtablö segebeite an Konischen Drehkörpern bei Hyperschallströmung. DLR, FB 71-77, Germany; 1971.
61. A.N. Antonov, and V.K. Grestov Unsteady separated supersonic flow over pointed and spiked bodies Fluid Dynamics 9 4 1974 578 582
62. A.N. Antonov, and V.K. Gretsov Experimental investigation of the characteristics of unsteady-state breakaway zones arising in a supersonic flow at a needle with a screen Fluid Dynamics 12 Number 4 1977 567 572
63. A.N. Antonov, and S.P. Shalaev Nonstationary separation on spiked bodies Fluid Dynamics 14 1 1979 71 76
64. A.N. Antonov, V.K. Gretsov, and S.P. Shalaev Nonsteady supersonic flow over spiked bodies Fluid Dynamics 11 5 September 1976 746 751
65. Kenworthy M. A study of unsteady axisymmetric separation in high speed flows. PhD dissertation, Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA; 1978.
66. A.G. Panaras Pulsating flows about symmetric concave bodies AIAA Journal 19 6 1981 804 806
67. Panaras AG. High speed unsteady separation about concave bodies - a physical explanation. Von Karaman Institute, Technical Note 123; 1977.
68. V.I. Zapryagaev, and S.G. Mironov Features of separated supersonic flow pulsations ahead of a spike-tipped cylinder Journal of Applied Mechanics and Technical Physics 32 6 1991 913 919
69. V.I. Zapryagaev, and I.N. Kavun Experimental study of the reverse flow in the forward separation region in a pulsating flow around a spiked body Journal of Applied Mechanics and Technical Physics 48 4 2007 492 500 (Pubitemid 47351297)
70. Shang JS, Hankey WL, Smith RE. Flow oscillations on spiked tipped bodies. AI AA paper 80-0062; 1980.
71. J.S. Shang, and W.L. Hankey Flow oscillations on spiked tipped bodies AIAA Journal 20 1 1982 25 26 (Pubitemid 12461818)
72. D. Feszty, K. Badcock, and B. Richards Driving mechanisms of high-speed unsteady spiked body flows, part 1: pulsation mode AIAA Journal 42 1 2004 95 106
73. D. Feszty, K. Badcock, and B. Richards Driving mechanisms of high-speed unsteady spiked body flows, part 2: oscillation mode AIAA Journal 42 1 2004 107 113
74. D. Feszty, K. Badcock, B. Richards, and M. Woodgate Numerical simulation of a pulsating flow arising over an axisymmetric spiked blunt body at Mach 2.21 and Mach 6.00 Shock Waves 10 5 2000 323 331
75. Feszty D, Badcock K, Richards B. Numerical simulation of the hysteresis phenomenon in high-speed spiked body flows. AIAA paper 2000-0141; 2000.
76. W.E. Thurman A flow-separation spike for hypersonic control of a hemisphere cylinder AIAA Journal 2 1 1964 159 161
77. E. Schulein Wave drag reduction concept for blunt bodies at high angles of attack, Shock waves 1 2009 Springer Berlin Heidelberg p. 1315320
78. V.S. Khlebnikov Effect of unsteady disturbances on the flow in a forward separation zone Fluid Dynamics 27 2 1992 294 297
79. V.S. Khlebnikov The influence of unsteady perturbations on the flow in a forward separation region upstream of a cone Fluid Dynamics 31 2 1996 274 283
80. V.S. Khlebnikov Effect of periodic disturbances on the flow in a nonsymmetric separation zone ahead of a blunt body Fluid Dynamics 31 5 1996 731 738 (Pubitemid 126707771)
81. Ahmed MYM. Aerothermodynamic design optimization of spiked hypersonic vehicles. PhD dissertation, Department of Mechanical Engineering, University of Sheffield, Sheffield, U.K.; 2010.
82. Fluent 6.3 User Guide, Fluent Inc., Lebanon, NH 03766, USA.
83. Gambit 2.4 User Guide, Fluent Inc., Lebanon, NH 03766, USA.
84. M. Ahmed, and N. Qin Drag reduction using aerodisks for hypersonic hemispherical bodies Journal of Spacecraft and Rockets 47 1 2010 62 80
85. Equations, tables, and charts for compressible flow. NACA TR 1135; 1953.
86. M. Ahmed, and N. Qin Numerical investigation of aeroheating characteristics of spiked blunt bodies at Mach 6 flight conditions The Aeronautical Journal 115 1165 2011
87. J.D. Anderson Fundamentals of aerodynamics Fourth Edition 2007 McGraw-Hill
88. Ahmed M, Qin N. Surrogate-based multi-objective aerothermodynamic design optimization of hypersonic spiked bodies. In: proceedings of the 28th International symposium on shock waves, Manchester; 1722 July 2011.
89. K. Deb, A. Pratap, S. Agarwal, and T. Meyarivan A fast and elitist multiobjective genetic algorithm: NSGA-II IEEE Transactions on Evolutionary Computation 6 2 2002 182 197 (Pubitemid 34555372)
90. NSGA-II toolbox for Matlab user guide. 〈http://www.mathworks.com/ matlabcentral/fileexchange/10429-nsga-ii-a-multi-objective-optimization- algorithm〉 (cited Jan. 2010).
91. Matlab 7 release 14 User Guide, The Mathworks Inc., USA.
92. M.D. Morris, and T.J. Mitchell Exploratory designs for computational experiments Journal of Statistical Planning and Inference 43 1995 381 402
93. J. Sacks, W.J. Welch, T.J. Mitchell, and H.P. Wynn Design and analysis of computer experiments Statistical Science 4 4 1989 409 423
94. Viana FAC. SURROGATES Toolbox Users Guide. 〈http://fchegury. googlepages.com〉, Cited December 2009.
95. N.V. Queipo, R.T. Haftka, W. Shyy, T. Goel, R. Vaidyanathan, and K. Tucker Surrogate-based analysis and optimization Progress in Aerospace Sciences 41 2005 1 28 (Pubitemid 40537187)
96. I.M. Sobol Global sensitivity indices for nonlinear mathematical models and their Monte Carlo estimates Mathematics and Computers in Simulation 55 2001 271 280 (Pubitemid 32672729)