Feasibility of a High-Performance Aerodynamic Impulse Facility
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[1] Clark H Lewis,et al. CHARTS OF NORMAL SHOCK WAVE PROPERTIES IN IMPERFECT NITROGEN (SUPPLEMENT: M SUB S = 1 TO 10) , 1964 .
[2] J. Lordi,et al. Nonequilibrium effects on high-enthalpy expansions of air. , 1965 .
[3] D. Spencer,et al. DEVELOPMENT OF 9000 K, 1400-ATM HOT-SHOT GAS SOURCE FOR PULSED MHD ACCELERATOR. , 1966 .
[4] C. E. Smith,et al. The starting process in a hypersonic nozzle , 1966, Journal of Fluid Mechanics.
[5] H. Mirels. Analytical solution for constant enthalpy mhd accelerator , 1964 .
[6] Comment on "Nonequilibrium Effects on High-Enthalpy Expansion of Air" , 1966 .
[7] C. J. Harris,et al. CORRELATION OF NONEQUILIBRIUM CHEMICAL PROPERTIES OF EXPANDING AIR FLOWS. , 1964 .
[8] J. Workman. Arc Structure in a Magnetic Annular Discharge , 1969 .
[9] Robert L. Trimpi,et al. A Preliminary Theoretical Study of the Expansion Tube, a New Device for Producing High-Enthalpy Short-Duration Hypersonic Gas Flows , 1962 .
[10] J. Spurk,et al. Simultaneous Streak and Frame Interferometry for Use in Short‐Duration Hypervelocity Facilities , 1965 .
[11] A. Hertzberg,et al. The Tailored-Interface Hypersonic Shock Tunnel , 1959 .
[12] J. H. Drake. Optimum isothermal acceleration of a plasma with constant magnetic field , 1963 .
[13] R. L. Leonard,et al. DESIGN AND OPERATION OF A LARGE PULSED JxB ACCELERATOR , 1965 .
[14] Glenn D. Norfleet,et al. A THEORETICAL REAL-GAS ANALYSIS OF THE EXPANSION TUNNEL , 1966 .
[15] J. Teare,et al. A STREAMTUBE APPROXIMATION FOR CALCULATION OF REACTION RATES IN THE INVISCID FLOW FIELD OF HYPERSONIC OBJECTS , 1961 .
[16] J. Lau. Electrical conductivity of inert gases-seed combination in shock tubes , 1964 .
[17] W. Powers,et al. Magnetic annular arc , 1962 .
[18] J. J. Givens,et al. Evaluation of flow properties in a combustion- driven expansion tube operating at 7.5 km/sec. , 1966 .
[19] A. Roshko. On Flow Duration in Low‐Pressure Shock Tubes , 1960 .
[20] J. J. Jones,et al. Exploratory study of performance of the Langley pilot model expansion tube with a hydrogen driver , 1966 .
[21] A. Schneiderman,et al. OPTIMIZATION OF THE THERMAL EFFICIENCY OF THE MAGNETIC ANNULAR ARC , 1966 .
[22] E. Pugh,et al. Laboratory simulation of solar wind phenomena. , 1965 .
[23] H. Mirels. Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer , 1964 .
[24] R. J. Stalker. An investigation of free piston compression of shock tube driver gas , 1961 .
[25] A. Schneiderman,et al. Performance characteristics of a magnetic annular arc. , 1966 .
[26] A. Seiff. A PROGRESS REPORT ON THE AMES HYPERVELOCITY FREE-FLIGHT FACILITIES AND SOME OF THE CURRENT RESEARCH PROBLEMS BEING STUDIED IN THEM , 1963 .
[27] Haught. SHOCK TUBE INVESTIGATION OF THE IONIZATION OF CESIUM VAPOR. Technical Report II-30 , 1962 .
[28] Clarence J. Harris. Comment on "Feasibility of a High-Performance Aerodynamic Impulse Facility" , 1968 .
[29] A. Schneiderman,et al. Axial current distribution in the exhaust of the magnetic annular arc. , 1966 .
[30] A. Hertzberg,et al. THE ISENTROPIC COMPRESSION TUBE: A NEW APPROACH TO GENERATING HYPERVELOCITY TEST FLOWS WITH LOW DISSOCIATION , 1967 .
[31] Jack D. Whitfield,et al. RESULTS OF AN EXPERIMENTAL INVESTIGATION OF THE PERFORMANCE OF AN EXPANSION TUBE , 1966 .
[32] Harold Mirels,et al. PERFORMANCE OF A 500-KJOULE MHD WIND TUNNEL. , 1968 .
[33] C. J. Harris,et al. THE DEVELOPMENT OF AN ELECTRICALLY HEATED SHOCK DRIVEN TEST FACILITY , 1962 .
[34] P. Rose,et al. Electric Arc-Driven Shock Tube , 1963 .
[35] Robert E. Mates,et al. A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack. , 1966 .
[36] Peter H. Rose,et al. ELECTRIC SHOCK TUBE FOR HIGH VELOCITY SIMULATION , 1962 .
[37] I. Bohachevsky,et al. A direct method for computation of nonequilibrium flows with detached shock waves. , 1965 .