Summary
A new operating condition has been designed for the High Enthalpy Shock Tunnel Göttingen (HEG). It corresponds to the free-flight conditions expected during the SHE-FEX and HYSHOT free-flight experiments and duplicates Mach 8 flight at 28 km altitude. The new operating condition was designed using a semi-analytic approach and then verified with an end-to-end facility simulation code.
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
H. Weihs, J. Longo, A. Gülhan, “The sharp edge flight experiment SHEFEX”, Proc. of the 4th European Workshop on Hot Structure and Thermal Protection Systems for Space Vehicles. Palermo, Italy, November 2002
R.J. Stalker: “Development of a hypervelocity wind tunnel”, Journal of the Royal Aeronautical Society, 76, pp. 374–384, 1972.
G. Eitelberg: “First results of the calibration and use of the HEG”, AIAA 1994–2525, 18th AIAA Aerospace Ground Testing Conference, Colorado Springs, June 20–23, 1994.
A. Paull: “Hypersonic airbreathing propulsion”. Paper 1620 presented at the 22nd International Symposium on Shock Waves, Imperial College, London, UK, July 18–23, 1999.
K. Hannemann, M. Schneider, B. Reimann, J. Martinez Schramm, “The influence and the delay of driver gas contamination in HEG” AIAA 2000–2595, 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, 19–22 June, 2000.
A. Paull, H. Alesi, S. Anderson: “HYSHOT flight program and how it was developed”. AIAA 2002–4939. AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France, September 29th- October 4th, 2002.
P.A. Jacobs: “LID: a computer program for the simulation of transient-flay facilities”. Dept. of Mechanical Engineering Report 1/99, University of Queensland, 1999.
P.A. Jacobs: “Quasi-one-dimensional modelling of a free-piston shock tunnel”, A.I.A.A. Journal 32 (1), pp. 137–145, 1994.
K. Hannemann, J. Martinez Schramm, S. Karl, W.H. Beck, “ Cylinder shock layer profiles measured in high enthalpy flays in HEG”, AIAA 2002–2913, 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, St Louis, June 24–28, 2002.
P.A. Jacobs, A.D. Gardner, K. Hannemann, “Gas-dynamic modelling of the HEG shock tunnel”, DLR-IB 224–2003A02.
M.K. McIntosh, “Computer program for the numerical calculation of frozen and equilibrium conditions in shock tunnels.” Department of Physics Unpublished Technical Report, Australian National University, Canberra, 1968.
T.J. McIntyre, C. Atcitty, “Pistons and Compression tubes-piston motions in the high-enthalpy shock tunnel (HEG)” DLR Internal report, DLR-IB 222–90A20, Institute of Experimental Flow Mechanics, DLR, Göttingen, 1991.
A.D. Gardner, “Calculation of low enthalpy conditions for the HEG”, DLR-IB 224–2003A03.
J.D. Anderson Jr, “Hypersonic and high temperature gas dynamics”, McGraw-Hill Inc, USA, 1989.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2004 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Gardner, A.D., Jacobs, P.A., Hannemann, K. (2004). End-to-end modelling and design of a new operating condition for HEG. In: Breitsamter, C., Laschka, B., Heinemann, HJ., Hilbig, R. (eds) New Results in Numerical and Experimental Fluid Mechanics IV. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 87. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-39604-8_28
Download citation
DOI: https://doi.org/10.1007/978-3-540-39604-8_28
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-53546-8
Online ISBN: 978-3-540-39604-8
eBook Packages: Springer Book Archive