Aerothermodynamic design of an inductively coupled plasma wind tunnel

32nd Thermophysics Conference

Volumn , Issue , 1997, Pages

  Bottin, Benoît ^a   Carbonaro, Mario ^a   Zemsch, Stefan ^a,b   Degrez, Gérard ^a  

^a VON KARMAN INSTITUTE FOR FLUID DYNAMICS   (Belgium)

^b BMW AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; CHEMICAL ANALYSIS; HIGH TEMPERATURE ENGINEERING; INDUCTIVELY COUPLED PLASMA; ONE DIMENSIONAL; SUPERSONIC AIRCRAFT; THERMODYNAMICS; WIND TUNNELS;

ANALYTIC EXPRESSIONS; CHEMICAL EQUILIBRIUMS; COMPUTER MODELING; HIGH TEMPERATURE AIR; QUASI-ONE DIMENSIONAL; STAGNATION POINT HEAT FLUXES; THERMODYNAMIC MODEL; VELOCITY GRADIENTS;

HEAT FLUX;

EID: 84964010176     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (44)

1. Crawford, R., Maus, J.R. “Aerodynamic and aerothermal facilities 2”, Methodology of hypersonic testing, VKI LS 1993-03, p. 6.16-6.26.
2. Babikian, D.S., Palumbo, G. “Measured and calculated spectral radiation from a blunt body shock layer in an arc-jet wind tunnel”, AIAA 94-0086, 1994.
3. taster, M.L., Arnold, J.O., Nichols, F., Horn, D. “Electric arc heaters”, AGARD high-enthalpy facility study group report, 1990.
4. Laure, S.H., Auweter-Kurtz, M., Fasoulas, S., Habiger, H.A., Rock, W.R. “The IRS plasma wind tunnels as a tool for the investigation of planet entry missions”, AIAA 92-3886, 1992.
5. Babat, G.I. “Electrodeless discharges and some allied problems”, Journal of the Institution of Electrical Engineers, part III, 94(27), January 1947, p. 27-37.
6. Boulos, M.I. “The inductively coupled Radio-Frequency plasma”, Journal of pure and applied chemistry, 57(9), 1985, p. 1321-1352.
7. Neiland, V.Ya. “Review of TsAGI wind tunnels”, Wind tunnels and wind tunnel test techniques, Southampton (UK), 1992.
8. Anfimov, N. “TsNIIMASH capabilities for aerogasdynamical and thermal testing of hypersonic vehicles”, AIM 92-3962, 1992.
9. Kolesnikov, A.F. “The aerothermodynamic simulation in suband supersonic high enthalpy jets: experiments and theory”, Second European Symposium on aerothermodynamics for space vehicles, ESA SP-367, 1995, p. 583-590.
10. Bottin, B., Carbonaro, M. “Potential applications of induction heating to aerospace technologies in the 1.2 MW plasmatron of the von Karman Institute”, Int. Congress of electromagnetic processing of materials, Paris La Defense, 1997. “
11. Bottin, B., Carbonaro, M., Deere, M., Mazauric, S., Novelli, A. “Design of a new inductively-coupled plasma wind tunnel for reentry material testing at the von Karman Institute”, Wind tunnels and wind tunnel test techniques, Cambridge (UK), 1997.
12. Bottin, B., Carbonaro, M. “The Plasmatron Project”, 85th Supersonic Tunnel Association meeting, Atlanta, 1996.
13. Anderson, J.D.Jr. “Hypersonic and high-temperature gas dynamics”, McGraw-Hill Book Company, New York, 1989.
14. Vincenti, W.G., Kruger, Ch. H Jr “Introduction to physical gas dynamics”, John Wiley and Sons, New York, 1965.
15. Park, C. “Nonequilibrium Hypersonic Aerothermodynamics”, John Wiley and Sons, New York, 1990.
16. Giordano, D., Marraffa, L. “Thermodynamic model of air in chemical equilibrium”, Theoretical and experimental methods in hypersonic flows, 70th AGARD fluid dynamics panel meeting and symposium, Italy, 1992.
17. Gordon, S., McBride, B.J. “A computer program for complex chemical equilibrium composition, rocket performance, incident and reflected shock, and Chapman-Jouguet detonations”, NASA SP-273, 1976.
18. Srinivasan, S., Tannehill, J., Weilmuenster, K.J. “Simplified curve fits for the thermodynamic properties of equilibrium air”, NASA RP-1181, 1987.
19. Bailey, H.E. “Programs for computing equilibrium thermodynamic properties of gases”, NASA TND-3921, 1967.
20. Gupta, R.N., Lee, K.-P., Thompson, R.A., Yos, J.M. “Calculations and curve fits of thermodynamic and transport properties for equilibrium air to 30000 K”, NASA RP-1260, 1991.
21. Bottin, B. “Pegase. Perfect gas equation solver for air at various pressures and temperatures. Version 2.4”, VKI IN 101, May 1996.
22. Cohen, N.B. “Correlation formulas and tables of density and some transport properties of equilibrium dissociating air for use in solutions of the boundary-layer equations”, NASA TN-D-194, 1960.
23. Lewis, C.H., Burgess, E.G.III. “Charts of sphere stagnation heattransfer rate in air and nitrogen at high temperatures”, AEDC TDR- 63-139, 1963.
24. Hilsenrath, J., Klein, M. “Tables of thermodynamic properties of air in chemical equilibrium including second virial corrections from 1500 to 15000 K”, AEDC TR-65-58, 1965.
25. Bruno, C. “Physico-chemical input data”, Aerothermochemistry for hypersonic technology, VKI LS 1995-04, 1995.
26. Hansen, Ch.F. “Approximations for the thermodynamic and transport properties of high-temperature air”, NASA TR R-50, 1959.
27. Murphy, A.B. “Transport coefficients of air, argon-air, nitrogenair and oxygen-air plasmas”, Plasma chemistry and plasma processing, 15(2), 1995, p. 279-307.
28. Vanden Abeele, D. “Computation of transport coefficients of air under slight deviations of equilibrium”, VKI IN 102, June 1996.
29. Devoto, R.S., Bauder, U.H., Cailleteau, J., Shires, E. “Air transport coefficients from electric arc measurements”, the Physics of Fluids, 21(4), 1978, p. 552-558.
30. Liepmann, H.W., Roshko, A. “Elements of gasdynamics”, John Wiley and Sons, New York, 1957.
31. Anderson, J.D Jr. “Modern compressible flow with historical perspective”, McGraw-Hill Book Company, New York, 1982.
32. Fay, J.A., Riddell, F.R. “Theory of stagnation point heat transfer in dissociated air”, Journal of the Aeronautical Sciences, 25(2), February 1958, p. 73-85.
33. Kolesnikov, A.F. “Conditions of simulation of stagnation point heat transfer from a high-enthalpy flow”. Fluid Mechanics, 1(1), January 1993.
34. Olivier, H., Gronig, H. “Hypersonic model testing in a shock tunnel”, AIAA 93-5004, 1993.
35. Truitt, R.W. “Fundamentals of aerodynamic heating”. The Ronald Press Company, New York, 1960.
36. Broglia, R., Manna, M., Deconinck, H., Degrez, G. “Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flows”, VKI TN 188, 1995.
37. Billig, F.S. “Shock-wave shapes around spherical- and cylindrical-nosed bodies”, Journal of Spacecraft and Rockets, 4(6), 1967, p. 822-823.
38. Yakushin, M.I. “Power requirements for the VKI plasmotron”, Contract report ENG-2, IPM, Moscow, 1995.
39. Kolesnikov, A.F., Yakushin, M.I. “Determination of heterogeneous recombination effective probabilities of atoms from heat fluxes to the surface in dissociated air flow”,Matematicheskoye Modelirovanie (in Russian), 1(3), 1989, p. 44-60.
40. Yakushin, M.I. “Report according to the contract n° 250049- 30476 between ESA & IPM RAS”, IPM, Moscow, April 1995.
41. Giilhan, A. “Computation of gas parameters for TPS-tests in LBK”, Private Communication, 1995.
42. Ames Research Staff, “Equations, tables and charts for compressible flow”, NASA report 1135, 1954.
43. Rival, P. “Private communication”, 1996.
44. Reboux, J., Delage, D., Riguet, C. “Les plasmas thermiques inductfis”, Revue Generate de Thermique, nb.310, October 1987, p. 534-541.