Recent developments in ramjets, ducted rockets and scramjets

Abstract The paper describes advances in ramjets, ducted rockets and scramjets that have taken place in the last decade. Particular attention is given to applications and test facilities.

[1]  D. W. Netzer,et al.  Combustion studies of metallized fuels for solid-fuel ramjets , 1986 .

[2]  A. Ferri,et al.  Review of scramjet propulsion technology. , 1968 .

[3]  Thomas J. Barber,et al.  Hypersonic vehicle propulsion - A computational fluid dynamics application case study , 1989 .

[4]  T. Tamaki,et al.  Feasibility study of air-breathing turbo-engines for horizontal take-off and landing space plane , 1989 .

[5]  D. Küchemann,et al.  Hypersonic aircraft and their aerodynamic problems , 1965 .

[6]  Frederick S. Billig,et al.  A procedure for optimizing the design of scramjet engines , 1978 .

[7]  Frank F. Webster Ramjet development testing - Which way is right? , 1989 .

[8]  Frederick S. Billig,et al.  A Procedure for Optimizing the Design of Scrainjet Engines , 1979 .

[9]  D. Netzer,et al.  Combustion Behavior of Solid-Fuel Ramjets , 1978 .

[10]  H. Grallert,et al.  Advanced air-breathing propulsion concepts for winged launch vehicles , 1989 .

[11]  F. Billig,et al.  Combustion Processes in Supersonic Flow , 1988 .

[12]  R. G. Morgan,et al.  Hypersonic combustion of hydrogen in a shock tunnel , 1989 .

[13]  Surya Pratap Vanka,et al.  Analytical characterization of flow fields in side-inlet dump combustors , 1983 .

[14]  Paul J. Waltrup,et al.  Liquid-fueled supersonic combustion ramjets - A research perspective , 1987 .

[15]  T. Nonweiler,et al.  Delta Wings of Shapes Amenable to Exact Shock-wave Theory , 1963, The Journal of the Royal Aeronautical Society.

[16]  S. Vanka,et al.  Investigation of a dual inlet side dump combustor using liquid fuel injection , 1985 .

[17]  David W. Netzer,et al.  Modeling Solid-Fuel Ramjet Combustion , 1977 .

[18]  Antonio Ferri,et al.  Review of Problems in Application of Supersonic Combustion , 1964, The Journal of the Royal Aeronautical Society.

[19]  J. Vos The calculation of turbulent reacting flows with a combustion model based on finite chemical kinetics , 1987 .

[20]  Daniel I. Sebacher,et al.  Langley Facility for Tests at Mach 7 of Subscale, Hydrogen-Burning, Airframe-Integratable, Scramjet Models , 1976 .

[21]  K. Schadow,et al.  Experimental Studies of Combustion Processes in a Tubular Combustor with Fuel Addition Along the Wall , 1978 .

[22]  G. Masuya,et al.  Experimental study on autoignition in a scramjet combustor , 1991 .

[23]  David L Kors,et al.  Combined cycle propulsion for hypersonic flight , 1988 .

[24]  J. Swithenbank Hypersonic air-breathing propulsion , 1967 .

[25]  G. Schulte,et al.  Temperature and Concentration Measurements in a Solid Fuel Ramjet Combustion Chamber , 1987 .

[26]  Surya Pratap Vanka,et al.  Mixing, chemical reaction, and flowfield development in ducted rockets , 1986 .

[27]  C. R. Peterson,et al.  Mechanics And Thermodynamics Of Propulsion , 1965 .

[28]  R. J. Stalker,et al.  Development of a hypervelocity wind tunnel , 1972, The Aeronautical Journal (1968).

[29]  R. J. Stalker,et al.  Scramjet testing in impulse facilities , 1987 .