Limiting Contractions for Starting Simple Ramp-Type Scramjet Intakes with Overboard Spillage

A method for obtaining the limiting contraction for supersonic intake-starting via overboard spillage is demonstrated for a simple ramp-type intake family. The strong-shock design principle is proposed on the basis of comparison of the limiting contraction line with the Kantrowitz (self-starting) lines of a few particular ramp intakes. Predicted starting characteristics compare favorably with two-dimensional inviscid numerical simulations.

[1]  Ryan P. Starkey,et al.  Axisymmetric Inlet Design for Combined-Cycle Engines , 2006 .

[2]  Arthur Kantrowitz,et al.  Preliminary Investigation of Supersonic Diffusers , 1945 .

[3]  W. J. D. Annand Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics. R. Hermann. Minneapolis Honeywell Co., Toronto. 378 pp. Illustrated. $16. , 1957 .

[4]  Michael K. Smart,et al.  Mach 4 Performance of Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition , 2004 .

[5]  Rudolf Hermann Supersonic inlet diffusers and introduction to internal aerodynamics , 1956 .

[6]  A. Shapiro The dynamics and thermodynamics of compressible fluid flow. , 1953 .

[7]  Rabi Tahir,et al.  Flow Starting in High Compression Hypersonic Air Inlets by Mass Spillage , 2004 .

[8]  Rabi Tahir,et al.  Analytical and Numerical Study of Flow Starting in Supersonic Inlets by Mass Spillage , 2007 .

[9]  S. Mölder,et al.  On stability of strong and weak reflected shocks , 2000 .

[10]  John C Evvard,et al.  The Use of Perforated Inlets for Efficient Supersonic Diffusion , 1956 .

[11]  Rabi Tahir,et al.  Unsteady Starting of High Mach Number Air Inlets -- A CFD Study , 2003 .

[12]  Arthur Kantrowitz,et al.  The Formation and Stability of Normal Shock Waves in Channel Flows , 1947 .

[13]  Kouichiro Tani,et al.  Effect of Sides-Spillage from Airframe on Scramjet Engine Performance , 2001 .

[14]  E. Timofeev,et al.  Development and Application of High-Resolution Adaptive Numerical Techniques in Shock Wave Research Center , 2001 .