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Numerical Solution of Supersonic Viscous Flow Over Blunt Delta Wings
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Turbulent Flow Over Vehicles at Angle of Attack
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March, also AIAA Paper 82-0027, 1982
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Prediction of Hypersonic Shock-Wave/Turbulent-Boundary-Layer Interaction Flows
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Calculation of Three-Dimensional Laminar and Turbulent Boundary Layers
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NASA SP-347
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Cebeci, T., Kaups, K., Ramsey, J., and Moser, A., “Calculation of Three-Dimensional Laminar and Turbulent Boundary Layers,” Aerodynamic Analysis Requiring Advanced Computers, NASA SP-347, 1975, pp. 41-76.
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Evaluation of Several Eddy Viscosity Models Through Comparison with Measurements in Hypersonic Flows
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Transitional and Turbulent Heat-Transfer Measurements on a Yawed Blunt Conical Nosetip
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Computation of Hypersonic Laminar, Transitional and/or Turbulent Viscous Flow Past Blunt Bodies at Angle of Attack
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Szema, K. Y. and Lewis, C. H., “Computation of Hypersonic Laminar, Transitional and/or Turbulent Viscous Flow Past Blunt Bodies at Angle of Attack,” Numerical Methods for Non-Linear Problems, Pineridge Press, Swansea, UK, 1980, pp. 873-884.
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Numerical Simulation of Supersonic and Hypersonic Turbulent Compression Corner Flows
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Computation of Supersonic Viscous Flows Over Ogive-Cylinders at Angle of Attack
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Paper 79-0131
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Rakich, J. V., Vigneron, Y. C., and Agarwal, R., “Computation of Supersonic Viscous Flows Over Ogive-Cylinders at Angle of Attack,” AIAA Paper 79-0131, 1979.
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An Evaluation of a Parabolized Navier-Stokes (PNS) Code for Cone-Cylinder-Flared Configurations
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Paper 84-2116
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PNS Computations for Spinning Shell at Moderate Angles of Attack and for Long L/D Finned Projectiles
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Paper 85-0273
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Computation of Turbulent Supersonic Flows Around Pointed Bodies Having Crossflow Separation
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Evaluation of Boundary Layer and Parabolized Navier-Stokes Solutions for Re-Entry Vehicles
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The Baldwin-Lomax Turbulence Model for Two-Dimensional Shock-Wave/Boundary-Layer Interactions
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Flow Over a Biconic Configuration with an Afterbody Compression Flap—A Comparative Numerical Study
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Supersonic Viscous Flow Over Cones at Incidence
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Tbilisi, USSR
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Measurements of the Three-Dimensional Boundary Layers on Conical Bodies at Mach 3 and Mach 5
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Ausherman, D. W., Yanta, W. J., and Rutledge, W. H., “Measurements of the Three-Dimensional Boundary Layers on Conical Bodies at Mach 3 and Mach 5,” AIAA Paper 83-1675, 1983.
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84968548952
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Heat Transfer, Surface Pressure and Flow Field Surveys on Conic and Biconic Models with Boundary Layer Trips at Mach 8—Phases IV and V
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Calspan/AEDC Div., Rept, TSR-80-V14
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Kaul, U. K. and Chaussee, D. S., “AWFAL Parabolized Navier-Stokes Code: 1983 AFWAL/NASA Merged Baseline Version,” U. S. Air Force Wright Aeronautical Lab., Wright-Patterson AFB, OH, AFWAL-TR-83-3118, 1983.
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