Design and Performance Analysis of a Supersonic Diffuser for Plasma Wing Tunnel

Plasma Wind Tunnels (PWT) are extensively used for screening and qualification of re-entry Thermel Protection System (TPS) materials. Proper design of a supersonic diffuser for plasma wind tunnel is of importance for achieving good pressurerecovery (thereby reducing vacuum pumping requirement & run time costs) and isolating downstream stream fluctuations from propagating costs) and isolating downstream stream fluctuationnts the details of a rapid design methodology successfully employed for designing supersonic diffuser for high power (several megawatts)plasma wind tunnels and numerical performance analysis of a diffuser configuration designed for one megawatt power rated plasma wind tunnel(enthalpy ~ 30 MJ/kg) using FLUENT 6.3® solver for different diffuser operating sub-atmospheric back-pressures.




References:
[1] J.D.Anderson. Jr., "Fundamentals of aerodynamics", McGraw-Hill, Inc,
2nd edition, 1991, pp. 522 - 527
[2] J.Lukasiewicz, "Diffusers for Supersonic Wind Tunnels", Journal of the
Aeronautical Sciences, Vol. 20 no.9, September 1953, pp. 617-626
[3] Alan Pope and Kennith L.Goin, " High-Speed Wind Tunnel Testing",
ROBERT E.KRIEGER PUBLISHING CO., INC, Reprinted Edition
1978, pp. 36 - 38
[4] G.J.Hanus, K.L.Mikkelsen, S.J.Olstad, "Supersonic Wind Tunnel
Diffuser Performance with High Model Blockage at Moderate to Low
Reynolds Numbers", AIAA 91-2274, June 1991
[5] P.J.Waltrup and F.S.Billig, "Structure of Shock Waves in Cylindrical
Ducts", AIAA Journal, Vol.11 no:10, October 1973, pp. 1404 - 1408
[6] William.H.Heiser and David.T.Pratt, "Hypersonic Air-breathing
Propulsion", AIAA, Educational series, 1994, pp. 251- 256
[7] R.K.Smith, D.A.Wagner, J.Cunningham and J.H.Painter, " High
Enthalpy Material Test Facility Design Improvements in Japan", AIAA
94-2592, June 1994
[8] T.J.Stahl, W.Winovich, G.Russo and S.Caristia, " Design and
Performance Characteristics of the CIRA Plasma Wind Tunnel", AIAA
91-2272, June 1991
[9] M.Capitelli, G.Colonna, C.Gorse and A.D-Angola, "Design and
Performance Characteristics of the CIRA Plasma Wind Tunnel", The
European Physical Journal D, pp. 279-289, 2000.
[10] Roop.N.Gupta, Kam-Pui Lee, R.A.Thomson and J.M.Yos, "
Calculations and curve fits of Thermodynamic and Transport properties
for Equilibrium air to 30000 oK", NASA Reference Publication 1260,
1991