Authors: PALMER GE HENLINE WD OLYNICK DR MILOS FS

Citation: Ge. Palmer et al., HIGH-FIDELITY THERMAL PROTECTION SYSTEM SIZING OF REUSABLE LAUNCH VEHICLE, Journal of spacecraft and rockets, 34(5), 1997, pp. 577-583

Authors: OLYNICK DR HENLINE WD

Citation: Dr. Olynick et Wd. Henline, NAVIER-STOKES HEATING CALCULATIONS FOR BENCHMARK THERMAL PROTECTION SYSTEM SIZING, Journal of spacecraft and rockets, 33(6), 1996, pp. 807-814

Authors: OLYNICK DR HENLINE WD CHAMBERS LH CANDLER GV

Citation: Dr. Olynick et al., COMPARISON OF COUPLED RADIATIVE FLOW SOLUTIONS WITH PROJECT FIRE-II FLIGHT DATA, Journal of thermophysics and heat transfer, 9(4), 1995, pp. 586-594

Authors: CHEN YK HENLINE WD TAUBER ME

Citation: Yk. Chen et al., MARS PATHFINDER TRAJECTORY BASED HEATING AND ABLATION CALCULATIONS, Journal of spacecraft and rockets, 32(2), 1995, pp. 225-230

Authors: CHEN YK HENLINE WD

Citation: Yk. Chen et Wd. Henline, HYPERSONIC NONEQUILIBRIUM NAVIER-STOKES SOLUTIONS OVER AN ABLATING GRAPHITE NOSETIP, Journal of spacecraft and rockets, 31(5), 1994, pp. 728-734