A survey of modern research in hypersonic aerodynamics

[1]  Paul Kutler,et al.  Shock-Capturing, Finite-Difference Approach to Supersonic Flows , 1971 .

[2]  Jr. J. D. Anderson,et al.  An engineering survey of radiating shock layers. , 1969 .

[3]  Y. Yamamoto,et al.  Floating shock fitting for three-dimensional inviscid supersonic flows , 1982 .

[4]  H. Harris Hamilton,et al.  Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type Configurations , 1972 .

[5]  J. P. Drummond,et al.  Supersonic flow over a rearward facing step with transverse nonreacting hydrogen injection , 1983 .

[6]  D. S. Chaussee,et al.  Computation of hypersonic viscous flow around three-dimensional bodies at high angles of attack , 1981 .

[7]  J. Philip Drummond,et al.  Numerical Study of Staged Fuel Injection for Supersonic Combustion , 1982 .

[8]  Paul Kutler,et al.  Computation of three-dimensional, inviscid supersonic flows , 1975 .

[9]  H. Harris Hamilton,et al.  Computation of Inviscid Flow Over Blunt Bodies Having Large Embedded Subsonic Regions , 1982 .

[10]  M. Rasmussen,et al.  Waverider Configurations Derived from Inclined Circular and Elliptic Cones , 1980 .

[11]  R. Davis,et al.  Numerical solution of the hypersonic viscous shock-layer equations , 1970 .

[12]  Dinesh K. Prabhu,et al.  Numerical solution of Space Shuttle Orbiter flowfield , 1984 .

[13]  F. G. Blottner,et al.  Chemical nonequilibrium boundary layer , 1964 .

[14]  L. H. Townend.  Research and design for lifting reentry , 1979 .

[15]  G. Moretti,et al.  A time-dependent computational method for blunt body flows. , 1966 .

[16]  Paul Kutler,et al.  Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference Schemes , 1973 .

[17]  B. Griffith,et al.  Hypersonic Mach number and real gas effects on Space Shuttle Orbiteraerodynamics , 1984 .

[18]  R. Lindsay,et al.  Elements of gasdynamics , 1957 .

[19]  P. M. Bainum,et al.  Motion of a Flexible Shallow Spherical Shell in Orbit , 1982 .

[20]  F. G. Blottner,et al.  Nonequilibrium laminar boundary-layer flow of ionized air , 1964 .

[21]  G. T. Coleman.  Aerodynamic Force Measurement on Caret and Delta Wings at High Incidence , 1973 .

[22]  G. Taylor.  The formation of a blast wave by a very intense explosion I. Theoretical discussion , 1950, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[23]  P S Epstein,et al.  On the Air Resistance of Projectiles. , 1931, Proceedings of the National Academy of Sciences of the United States of America.