AAAAAA

   
Results: 1-5 |
Results: 5

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: OLYNICK DR TAYLOR JC HASSAN HA
Citation: Dr. Olynick et al., COMPARISONS BETWEEN MONTE-CARLO METHODS AND NAVIER-STOKES EQUATIONS FOR REENTRY FLOWS, Journal of thermophysics and heat transfer, 8(2), 1994, pp. 251-258

Authors: HASSAN B CANDLER GV OLYNICK DR
Citation: B. Hassan et al., THERMOCHEMICAL NONEQUILIBRIUM EFFECTS ON THE AEROTHERMODYNAMICS OF AEROBRAKING VEHICLES, Journal of spacecraft and rockets, 30(6), 1993, pp. 647-655
Risultati: 1-5 |