Summary
Steady, hypersonic viscous flows over two-dimensional compression ramps are computed. In order to gain insight into the influence of different Mach numbers, Reynolds numbers and ramp angles on the flow structure, results are presented for low and high Mach numbers, for low and high Reynolds numbers as well as for different ramp angles. Furthermore, with respect to high Mach number flows, the influence of real gas effects is investigated. Computed surface pressure, skin friction and heat transfer distributions are compared with available measurements.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Hung, C.M., MacCormack, R.W.: “Numerical Solutions of Supersonic and Hypersonic Laminar Flows over a Two-Dimensional Compression Corner”, AIAA Journal, Vol. 14, April 1976.
Stokesberry, D.C., Tannehill, J.C.: “Computation of Separated Flow on a Ramp Using the Space Marching Conservative Supra-Characteristics Method”, AIAA Paper 86-0564, Jan. 1986.
Lawrence, S.L., Tannehill, J.C., Chaussee, D.S.: “An Upwind Algorithm for the Pa-rabolized Navier-Stokes Equations”, AIAA Paper 86-1117, May 1986.
Ginoux, J.J., “On Some Properties of Reattaching Laminar and Transitional High Speed Flows”, von Karman Institute, Technical Note 53, September 1969.
Holden, M.S., Moselle, J.R.: “Theoretical and Experimental Studies of the Shock Wave-Boundary Layer Interaction on Compression Surfaces in Hypersonic Flows”, CALSPAN Report AF-2410-A-1, October 1969.
Haase, W., Wagner, B., Jameson, A.: “Development of a Navier-Stokes Method Based on a Finite Volume Technique for the Unsteady Euler Equations”, Notes on Numerical Fluid Mechanics, Vol. 7, pp. 99–108, Vieweg Verlag, Braunschweig, 1984.
Tannehill, J.C., Mugge, P.H.: “Improved Curve Fits for the Thermodynamic Properties of Equilibrium Air Suitable for Numerical Computation Using Time-Dependent or Shock-Capturing Methods”, NASA CR-2470, October 1974.
Jameson, A., Schmidt, W., Turkel, E.: “Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time Stepping Scheme”, AIAA Paper 81-1259, 1981.
Seibert, W., Fritz, W., Leicher, S.: “On the Way to an Integrated Mesh Generation System for Industrial Applications”, AGARD Fluid Dynamics Panel Specialists’ Meeting on “Applications of Mesh Generation to Complex 3-D Configurations, Loen, Norway, May 1989.
Author information
Authors and Affiliations
Editor information
Rights and permissions
Copyright information
© 1990 Springer Fachmedien Wiesbaden
About this paper
Cite this paper
Haase, W. (1990). Viscous, Hypersonic Flows Over Compression Ramps. In: Wesseling, P. (eds) Proceedings of the Eighth GAMM-Conference on Numerical Methods in Fluid Mechanics. Notes on Numerical Fluid Mechanics (NNFM), vol 29. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-663-13975-1_20
Download citation
DOI: https://doi.org/10.1007/978-3-663-13975-1_20
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-528-07629-0
Online ISBN: 978-3-663-13975-1
eBook Packages: Springer Book Archive