An Accurate Prediction of Surface Temperature History in a Supersonic Flight
Authors: A. M. Tahsini, S. A. Hosseini
Abstract:
In the present study, the surface temperature history of the adaptor part in a two-stage supersonic launch vehicle is accurately predicted. The full Navier-Stokes equations are used to estimate the aerodynamic heat flux and the one-dimensional heat conduction in solid phase is used to compute the temperature history. The instantaneous surface temperature is used to improve the applied heat flux, to improve the accuracy of the results.
Keywords: Aerodynamic heating, Heat conduction, Numerical simulation, Supersonic flight, Launch vehicle.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1089106
Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1711References:
[1] C. J. Riley, and F. R. Dejarnette, "Engineering aerodynamic heating method for hypersonic flow," Journal of Spacecraft and Rockets, Vol. 29, No. 3, pp. 327-339, 1992.
[2] C. Shaw, Y. Y. Shan, N. Qin, "Development of a Local MQ-DQ-Based Stencil Adaptive Method and its Application to Solve Incompressible Navier-Stokes Equations," Int. J. Numer. Meth. Fluids, Volume 55, Issue 4, pp. 367–386, 2007.
[3] C. Shaw, and N. Qin, "Solution of the Navier-Stokes Equations for the Flow around an Aerofoil in Oscillating Free Stream," Proceeding of the 20th Congress of the International Council of the Aeronautical Sciences, ICAS, Vol.1, pp19-29. ISBN 1-56347-219-8, 1996.
[4] S. L. Lawrence, D. S. Chaussee, and J. C. Tannehill, "Application of an Upwind Algorithm to the Three-Dimensional Parabolized Navier-Stokes Equations," AIAA paper 87-1112-CP, June 1987.
[5] T. Birch, S. Prince, D. K. Ludlow, and N. Qin, "The Application of a Parabolized Navier-Stokes Solver to Some Hypersonic Flow Problems," AIAA 2001-1753.
[6] S. Noori, S. Ghasemloo and M. Mani, "A New Method for Solution of Viscous Shock Layer Equations" Journal of Aerospace Engineering, Vol. 224, 2010.
[7] Truitt, Robert W., "Fundamentals of Aerodynamic Heating," Ronald Press, 1960.
[8] E. V. Zoby, J. J. Moss, and K. Sutton, "Approximate Convective-Heating Equations for Hypersonic Flows," Journal of Spacecraft and Rockets, Vol. 18, No.1, pp.64-70, 1981.