Authors: WEILMUENSTER KJ GNOFFO PA GREENE FA RILEY CJ HAMILTON HH

Citation: Kj. Weilmuenster et al., HYPERSONIC THERMAL ENVIRONMENT OF A PROPOSED SINGLE-STAGE-TO-ORBIT VEHICLE, Journal of spacecraft and rockets, 34(6), 1997, pp. 697-704

Authors: WEILMUENSTER KJ GNOFFO PA GREENE FA RILEY CJ HAMILTON HH ALTER SJ

Citation: Kj. Weilmuenster et al., HYPERSONIC AERODYNAMIC CHARACTERISTICS OF A PROPOSED SINGLE-STAGE-TO-ORBIT VEHICLE, Journal of spacecraft and rockets, 33(4), 1996, pp. 463-469

Authors: GREENE FA

Citation: Fa. Greene, APPLICATION OF THE MULTIGRID SOLUTION TECHNIQUE TO HYPERSONIC ENTRY VEHICLES, Journal of spacecraft and rockets, 31(5), 1994, pp. 744-750

Authors: HAMILTON HH GREENE FA

Citation: Hh. Hamilton et Fa. Greene, APPROXIMATE METHOD FOR CALCULATING HEATING RATES ON 3-DIMENSIONAL VEHICLES, Journal of spacecraft and rockets, 31(3), 1994, pp. 345-354

Authors: WEILMUENSTER KJ GNOFFO PA GREENE FA

Citation: Kj. Weilmuenster et al., NAVIER-STOKES SIMULATIONS OF ORBITER AERODYNAMIC CHARACTERISTICS INCLUDING PITCH TRIM AND BODYFLAP, Journal of spacecraft and rockets, 31(3), 1994, pp. 355-366

Authors: WEILMUENSTER KJ GREENE FA

Citation: Kj. Weilmuenster et Fa. Greene, HL-20 COMPUTATIONAL FLUID-DYNAMICS ANALYSIS, Journal of spacecraft and rockets, 30(5), 1993, pp. 558-566