D. Olynick

发表

Hypersonic flow simulations using a diagonal implicit method

G. Candler, D. Olynick, 1991 .

Comparison of Coupled Radiative Navier-Stokes Flow Solutions with the Project Fire II Flight Data

W. Henline, G. Candler, D. Olynick, 1994 .

Comparisons between Monte Carlo methods and Navier-Stokes equations for re-entry flows

Jeff C. Taylor, H. Hassan, D. Olynick, 1994 .

Upwind methods for ionized flows

Jeff C. Taylor, H. Hassan, D. Olynick, 1994 .

Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles

Graham V. Candler, Basil Hassan, David R. Olynick, 1993 .

The effect of thermo-chemical nonequilibrium on the aerodynamics of aerobraking vehicles

Graham V. Candler, David R. Olynick, G. Candler, 1992 .

Computational Aerothermodynamic Design Issues for Hypersonic Vehicles

Ethiraj Venkatapathy, H. Harris Hamilton, K. James Weilmuenster, 1997 .

Aerothermodynamic heating analysis and heatshield design of an SSTO rocket vehicle for Access-to-Space

David R. Olynick, William D. Henline, W. Henline, 1995 .

AEROTHERMODYNAMICS OF THE STARDUST SAMPLE RETURN CAPSULE

Michael E. Tauber, David R. Olynick, Yih-Kanq Chen, 1998 .

High-Fidelity Thermal Protection System Sizing of Reusable Launch Vehicle

Grant Palmer, Frank S. Milos, David R. Olynick, 1997 .

Forebody TPS sizing with radiation and ablation for the Stardust Sample Return Capsule

Yih-Kanq Chen, Michael Tauber, M. Tauber, 1997 .

Current Grid Generation Strategies and Future Requirements in Hypersonic Vehicle Design, Analysis and Testing

Dinesh K. Prabhu, Ethiraj Venkatapathy, Periklis Papadopoulos, 1999 .

Comparison of coupled radiative flow solutions with Project Fire II flight data

Graham V. Candler, Lin Hartung Chambers, David R. Olynick, 1995 .

Navier-Stokes Heating Calculations for Benchmark Thermal Protection System Sizing

David R. Olynick, William D. Henline, W. Henline, 1996 .

TPS requirements for advanced sample return capsule design

Yih-Kanq Chen, H. Tran, D. Olynick, 1998 .

Trajectory-Based Thermal Protection System Sizing for an X-33 Winged Vehicle Concept

David R. Olynick, D. Olynick, 1998 .

Trajectory based validation of the Shuttle heating environment

Dave Olynick, Tim Tam, D. Olynick, 1996 .

Importance of 3-D grid resolution and structure for calculating reentry heating environments

David R. Olynick, D. Olynick, 1996 .

for Advanced Sample Return Capsule Design

Paul F. Wercinski, Dave Olynick, Huy Tran, 1998 .

Wake flow calculations with ablation for the Stardust Sample Return Capsule

Yih-Kanq Chen, Michael Tauber, M. Tauber, 1997 .

Three-dimensional hypersonic flowfields and heating analysis over DC-3 vehicle

D. Olynick, G. Palmer, Chen ine W D Y-KHenline, 1995 .

Numerical benchmarks for Navier-Stokes heating calculations on Access-to-Space vehicles

David Olynick, William D. Henline, W. Henline, 1995 .

A heating analysis and thermal protection system sizing of a lifting body single-stage-to-orbit vehicle

Grant Palmer, Frank S. Milos, David R. Olynick, 1995 .

CFD code comparisons for Mars entry simulations

Dinesh K. Prabhu, Periklis Papadopoulos, Yih-Kanq Chen, 1998 .

Comparisons between DSMC and the Navier-Stokes equations for reentry flows

Hassan Hassan, Jeff C. Taylor, David R. Olynick, 1993 .