Computational Aerothermodynamic Design Issues for Hypersonic Vehicles von Gnoffo, Peter A, Weilmuenster, K. James, Hamilton, H. Harris, Olynick, David R, Venkatapathy, Ethiraj

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X-38 Experimental Aeroheating at Mach 10 von Berry, Scott A, Horvath, Thomas J, Weilmuenster, K. James, Alter, Stephen J, Merski, N. Ronald

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Prediction and Validation of Mars Pathfinder Hypersonic Aerodynamic Database von Gnoffo, Peter A, Braun, Robert D, Weilmuenster, K. James, Mitcheltree, Robert A, Engelund, Walter C, Powell, Richard W

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Numerical analysis and simulation of an assured crew return vehicle flow field / K. James Weilmuenster, Robert E. Smith, Jr., and Francis A. Greene von Weilmuenster, K. James

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Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data / K. James Weilmuenster and H. Harris Hamilton II von Weilmuenster, K. James

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A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies / K. James Weilmuenster and H. Harris Hamilton II von Weilmuenster, K. James

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A finite-difference analysis of the nozzle starting process in an expansion tunnel / K. James Weilmuenster von Weilmuenster, K. James

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An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube / by K. James Weilmuenster von Weilmuenster, K. James

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High angle-of-attack inviscid Shuttle Orbiter computation von Kleb, William L, Weilmuenster, K. James

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Application of axisymmetric analog for calculating heating in three-dimensional flows von Hamilton, H. Harris, DeJarnette, Fred R, Weilmuenster, K. James

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Navier-Stokes simulations of Orbiter aerodynamic characteristics including pitch trim and bodyflap von Weilmuenster, K. James, Gnoffo, Peter A, Greene, Francis A

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A review of some approximate methods used in aerodynamic heating analyses von DeJarnette, Fred R, Hamilton, H. Harris, Weilmuenster, K. James, Cheatwood, F. McNeil

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Computed and experimental surface pressure and heating on 70-deg sphere cones von Weilmuenster, K. James, Hamilton, H. Harris

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HL-20 computational fluid dynamics analysis von Weilmuenster, K. James, Greene, Francis A

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User's guide for vectorized code EQUIL for calculating equilibrium chemistry on Control Data STAR-100 computer / Ajay Kumar, Randolph A. Graves, Jr., and K. James Weilmuenster von Kumar, Ajay

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Hypersonic Thermal Environment of a Proposed Single-Stage-to-Orbit Vehicle von Weilmuenster, K. James, Gnoffo, P. A, Greene, F. A, Riley, C. J, Hamilton, H. H

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Comparison of Shuttle Flight Pressure Data to Computational and Wind-Tunnel Results von Bradley, P.F, Siemers, P.M, Weilmuenster, K. James

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Aeroassisted Flight Experiment aerodynamic characteristics at flightconditions von Weilmuenster, K. James, Gnoffo, Peter A

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Influence of sonic-line location on Mars Pathfinder Probe aerothermodynamics von Gnoffo, Peter A, Weilmuenster, K. James, Braun, Robert D, Cruz, Christopher I

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X-38 experimental aeroheating at Mach 10 von Berry, Scott A, Horvath, Thomas J, Weilmuenster, K James, Alter, Stephen J, Merski Jr., N. Ronald

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