- Manigandan, S. and Sruthisree, K. N. “Numerical Analysis of Slotted Aerospike for Drag Reduction”, International Conference on Recent Advances in Fluid and Thermal Sciences, 2019.##
- Anderson, J. D. “Hypersonic and High-Temperature Gas Dynamics”, AIAA, 2006.##
- Shashank, K., Suzuki, K., and Rathakrishnan, E. “Effect of Vortex-Size Around Spike Root and Body Base on Possible Hypersonic Drag Reduction”, The Seventh International Colloquium on Bluff Body Aerodynamics and Applications, Shanghai, China, 2012.##
- Menezes, V., Saravanan, S., and Reddy, K. P. J. “Shock Tunnel Study of Spiked Aerodynamic Bodies Flying at Hypersonic Mach Number”, Shock Waves, Vol. 12, No. 3, pp.197-204, 2002.##
- McMahon, H. M. “An Experimental Study of the Effect of Mass Ejection at the Stagnation Point of a Blunt Body”, Memo. Hypersonic Res. Project, No.42, 1959.##
- Meyer, B., Nelson, H. F., and Riggins, D. W. “Hypersonic Drag and Heat-Transfer Reduction Using a Forward-Facing Jet”, J. Aircr, Vol. 38, pp.680-686, 2001.##
- Riggins, D. W., Nelson, H. F., and Johnson, E. “Blunt-Body Wave Drag Reduction Using Focused Energy Deposition”, AIAA J, Vol. 37, No. 4, pp. 460-467, 1999.##
- Marsh, J. J., Myrabo, L. N., Messitt, D. G., And Nagamatsu, H. T. “Experimental Investigation of the Hypersonic air Spike inlet at Mach 10”, 34th Aerospace Sciences Meeting and Exhibit, 1996.##
- Haibo, L. and Liu, W. “Nummerical Simulation in Influence of Forward-Facing Cavity on Aerodynamic Heating of Hypersonic Vehicle”, Procedia Eng, Vol. 29, pp.4096-4100, 2012.##
- Rajesh, Y. and Guven, U. “Aerodynamic Heating of a Hypersonic Projectile with Forward-Facing Ellipsoid Cavity at Nose”, J. Spacecr. Rockets, Vol. 52, No. 1, pp.157-165, 2015.##
- ajesh, Y. And Guven, U. “Aerothermodynamics of a Hypersonic Vehicle with a Forward Facing Parabolic Cavity at Nose”, Proc. Inst. Mech. Eng., Part G, pp.1863-1874, 2015.##
- Bogdonoff, S. M. and Irwin, E. V. “Preliminary Investigations of Spiked Bodies at Hypersonic Speeds”, J. Aerosp. Sci, Vol. 26, No. 2, pp.65-74, 1959.##
- Mehta, R. “Flow Field Computations over Conical, Disc and Flat Spiked Body at Mach 6”, 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, 2009.##
- Schnepf, C. h., Wysocki, O., and Schülein, E. “Wave Drag Reduction Due to a Self-Aligning Aerodisk”, Progress in Flight Physics, Vol. 7, pp.475-488, 2015.##
- Gerdroodbary, M. B. and Hosseinalipour, S. M. “Numerical Simulation of Hypersonic Flow over Highly Blunted Cones with Spike”, Acta Astronaut, Vol. 67, pp.180-193, 2010.##
- Schülein, E. “Wave Drag Reduction Approach for Blunt Bodies at High Angles of Attack: Proof-Of-Concept Experiments”, 4th Flow Control Conference, 2008.##
- Ahmed, M. Y. M. and Qin, N. “Recent Advances in the Aerothermodynamics of Spiked Hypersonic Vehicles”, Prog. Aerosp. Sci, Vol. 47, pp.425-449, 2011.##
- Kalimuthu, R. and Rathakrishnan, E. “Aerospike for Drag Reduction in Hypersonic Flow”, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008.##
- Yamauchi, M., Fujii, K., and Higashino, F. “Numerical Investigation of Supersonic Flows around a Spiked Blunt Body”, J. Spacecr. Rockets, Vol. 32, pp.32-42, 1995.##
- Hutt, G. R., and Howe, A. J. “Forward Facing Spike Effects on Bodies of Different Cross Section in Supersonic Flow”, Aeronaut. J, Vol. 93, pp.229-234, 1989.##
- Ahmed, M. Y. M. and Qin, N. “Metamodels for Aerothermodynamic Design Optimization of Hypersonic Spiked Blunt Bodies”, Aerosp. Sci. Technol, Vol. 14, pp.364-376, 2010.##
- Crawford, D. H. “Investigation of the Flow over a Spiked-Nose Hemisphere-Cylinder at a Mach Number of 6.8”, NASA/TM, 1959.##
- Motoyama, N., Mihara, K., Miyajima, R., Watanuki, T., and Kubota, H. “Thermal Protection and Drag Reduction with Use of Spike in Hypersonic Flow”, 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference, 2001.##
- Kalimuthu, R., Mehta, R. C., and Rathakrishnan, E. “Experimental Investigation on Spiked Body in Hypersonic Flow”, Aeronaut. J, Vol. 112, pp.593-598, 2008.##
- Ajmal, M., Durrani, N., and Saeed, H. A. “Design of Spiked Hemispherical Body in Hypersonic Flow”, 12th International Bhurban Conference on Applied Sciences and Technology, pp. 453-459, 2015.##
- Wang, Z. G., Sun, X.W., Huang, W., Li, S. B., and Yan, L. “Experimental Investigation on Drag and Heat Flux Reduction in Supersonic/Hypersonic Flows: a Survey”, Acta Astronaut, Vol. 129, pp.95-110, 2016.##
- Schnepf, C., Wysocki, O., and Schülein, E. “Wave Drag Reduction with a Self-Aligning Aerodisk on a Missile Configuration”, Progress in Flight Physics, Vol. 9, pp.149-172, 2017.##
- Ahmed, M. Y. M. and Qin, N. “Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies”, J. Spacecr. Rockets, Vol. 47, pp.62-80, 2010.##
- Kulkarni, V., Menezes, V. and Reddy, K. P. J. “Effectiveness of Aerospike for Drag Reduction on a Blunt Cone in Hypersonic Flow”, J. Spacecr. Rockets, Vol. 47, pp.542-544, 2010.##
- Tahani, M., Karimi, M. S., Motlagh, A. M., and Mirmahdian, S. “Numerical Investigation of Drag and Heat Reduction in Hypersonic Spiked Blunt Bodies”, Heat Mass Transfer, Vol. 49, pp. 1369-1384, 2013.##
- Huebner, L., Anthony, M., and Boudreaux, E. “Experimental Results on the Feasibility of an Aerospike for Hypersonic Missiles”, 33rd Aerospace sciences meeting and exhibit, 1995.##
- Hasani, M., Haghiri, A., and Islamy, M. “Investigation of Spike Length on Wave Drag Reduction of Standard Model in Hypersonic Flow”, J. Solid Fluid Mechanics, Vol. 10, pp.177-192, 2020. (In Persian)##
- Bertin, J. J. “Advances in Hypersonies- Volume 1 Defining the Hypersonic Environment”, Springer Science+Business Media, New York, 1992.##
- Gray, J. D. “Summary Report on Aerodynamic Characteristics of Standard Models HB-1 and HB-2”, Arnold Engineering Development Center Arnold, Afb Tn, 1964.##
- Standard, British. “General Requirements For The Competence of Testing and Calibration Laboratories”, EN ISO/IEC 17025 , 2006.##
- Kalimuthu, R. and Rathakrishnan, E. “Aerospike for Drag Reduction in Hypersonic Flow”, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008.##
|