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Original Articles

Aerothermodynamic shape optimization of hypersonic blunt bodies

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Pages 909-926 | Received 11 Aug 2013, Accepted 27 May 2014, Published online: 10 Jul 2014

References

  • Ahmed, M. Y. M., and N. Qin. 2012. “Surrogate-Based Multi-Objective Aerothermodynamic Design Optimization of Hypersonic Spiked Bodies.” AIAA Journal 50: 797–810. doi: 10.2514/1.J051018
  • Baldwin, B., and H. Lomax. 1978. “Thin-layer approximation and algebraic model for separated turbulent flows.” AIAA Article 1978-257.
  • Candler, G. 1988. The computation of weakly ionized hypersonic flows in thermochemical nonequilibrium (PhD diss.). Stanford University.
  • Cui, K., and S.-C. Hu. 2013. “Shape design to minimize the peak heat-flux of blunt leading-edge.” AIAA Article 2013–0233.
  • Cui, K., S.-C. Hu, T.-Y. Gao, X.-P. Wang, and G.-W. Yang. 2011. “Leading edge aerothermal inverse design of hypersonic vehicle based on homotopy optimization method.” Proceedings of the Sixth International Conference on Fluid Mechanics 1376: 172–174.
  • Davis, T. 2003. UMFPACK Version 4.1 User Manual. University of Florida.
  • Desideri, J.-A., B. A. El Majd, and A. Janka. 2007. “Nested and self-adaptive Bezier parameterizations for shape optimization.” Journal of Computational Physics 224: 117–131. doi: 10.1016/j.jcp.2006.12.016
  • Eyi, S. 2012. “Convergence Error and Higher-Order Sensitivity Estimations.” AIAA Journal 50: 2219–2234. doi: 10.2514/1.J051592
  • Eyi, S., and M. Yumusak. 2012. “Design optimization in hypersonic flows.” AIAA Article 2012–5827.
  • Fletcher, R., and C. M. Reeves. 1964. “Function minimization by conjugate gradients.” Computer Journal 7: 149–154. doi: 10.1093/comjnl/7.2.149
  • Gupta, R., J. M. Yos, R. A. Thompson, and K. P. Lee. 1990. A review of reaction rates and thermodynamic and transport for an 11-species air model for chemical and thermal non-equilibrium calculations to 30000K (NASA Report No. RP-1232).
  • JANAF Thermochemical Tables. 1971. NBS-NSRDS, 37.
  • Kim, K.-H., H.-O. Rho, and C. Park. 2000. “Navier–Stokes computation of flows in arc heaters.” Journal of Thermophysics and Heat Transfer 14: 250–258. doi: 10.2514/2.6516
  • Kliche, D., C. Mundt, and E. H. Hirschel. 2011. “The hypersonic mach number independence principle in the case of viscous flow.” Shock Waves 21: 307–314. doi: 10.1007/s00193-011-0318-y
  • Lee, J.-W., B.-Y. Min, Y.-H. Byun, and S.-J. Kim. 2006. “Multipoint nose shape optimization of space launcher using response surface method.” Journal of Spacecraft and Rockets 43: 137–146. doi: 10.2514/1.11228
  • Lees, L. 1956. “Laminar heat transfer over blunt-nosed bodies at hypersonic flight speeds.” Journal of Jet Propulsion 26: 259–269. doi: 10.2514/8.6977
  • Lobb, R. 1962. “Experimental measurement of shock detachment distance on spheres fired in air at hypervelocities.” AD0284378, Naval Ordnance Lab.
  • Meyer, B., H. F. Nelson, and D. W. Riggins. 2001. “Hypersonic drag and heat-transfer reduction using a forward-facing jet.” Journal of Aircraft 38: 680–686. doi: 10.2514/2.2819
  • Najm, H. N., P. S. Wyckoff, and Omar M. Knioy. 1998. “A semi-implicit numerical scheme for reacting flow I. stiff chemistry.” Journal of Computational Physics 143: 381–402. doi: 10.1006/jcph.1997.5856
  • Oswatitsch, K. 1951. “Ähnlichkeitsgesetz für Hyperschallströmung.” ZAMP 2: 249–264. doi: 10.1007/BF02579688
  • Park, C. 1985. “On convergence of computation of chemically reacting flows.” AIAA Article 85–0247.
  • Park, C. 1990. Nonequilibrium Hypersonic Aerothermodynamics, 5–13. New York: Wiley.
  • Parsons, N., X. Zhong, J. Kim, and J. Eldredge. 2010. “Numerical study of hypersonic receptivity with thermochemical non-equilibrium on a blunt cone.” AIAA Article 2010–4446.
  • Riggins, D., H. F. Nelson, and E. Johnson. 1999. “Blunt-body wave drag reduction using focused energy deposition.” AIAA Journal 37: 460–467. doi: 10.2514/2.756
  • Rodi, P. 2013. “Optimization of Bezier curves for high speed leading edge geometries.” AIAA Article 2013–1004.
  • Rose, P. H., and J. O. Stankevics. 1963. “Stagnation point heat transfer measurements in partially ionized air.” AIAA Journal 1: 2752–2763. doi: 10.2514/3.2169
  • Roy, C. J., and F. G. Blottner. 2006. “Review and assessment of turbulence models for hypersonic flows.” Progress in Aerospace Sciences 42: 469–530. doi: 10.1016/j.paerosci.2006.12.002
  • Sarma, G. 2000. “Physico-chemical modelling in hypersonic flow simulation.” Progress of Aerospace Science 36: 281–330. doi: 10.1016/S0376-0421(00)00004-X
  • Schenk, O., M. Bollhoefer, and R. Roemer. 2008. “On large-scale diagonalization techniques for the Anderson model of localization.” SIAM Review 50: 91–112. doi: 10.1137/070707002
  • Silton, S. I., and D. B. Goldstein. 2005. “Use of an axial nose-tip cavity for delaying ablation onset in hypersonic flow.” Journal of Fluid Mechanics 528: 297–321. doi: 10.1017/S0022112004002460
  • Squire, W., and G. Trapp. 1998. “Using complex variables to estimate derivatives of real functions.” SIAM Review 40: 110–112. doi: 10.1137/S003614459631241X
  • Van Albada, G., B. Van Leer, and W. W. Roberts. 1982. “A comparative study of computational methods in cosmic gas dynamics.” Astronomy and Astrophysics 108: 76–84.
  • Van Leer, B. 1979. “Towards the ultimate conservative difference scheme, V. a second order sequel to Godunov's method.” Journal of Computational Physics 32: 101–136. doi: 10.1016/0021-9991(79)90145-1
  • Wright, M., M. Loomis, and P. Papadopoulos. 2003. “Aerothermal analysis of the project FIRE II afterbody flow.” Journal of Thermophysics and Heat Transfer 17: 240–249. doi: 10.2514/2.6757
  • Yisheng, R. 2013. “Drag reduction research in supersonic flow with opposing jet.” Acta Astronautica 91: 1–7. doi: 10.1016/j.actaastro.2013.04.015
  • Yumusak, M., and S. Eyi. 2012. “Design optimization of rocket nozzles in chemically reacting flows.” Computers and Fluids 65: 25–34. doi: 10.1016/j.compfluid.2012.05.002
  • Zeitoun, D., E. Schall, Y. Burtschell, and M. C. Druguet. 1995. “Vibration–dissociation coupling in nonequilibrium hypersonic viscous flows.” AIAA Journal 33: 765–788. doi: 10.2514/3.12335

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