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Results: 1-11 |
Results: 11
EXPERIMENTAL-ANALYSIS OF THE TURBULENT SHEAR STRESSES FOR DISTORTED SUPERSONIC BOUNDARY-LAYERS
Authors: LUKER JJ HALE CS BOWERSOX RDW
Citation: Jj. Luker et al., EXPERIMENTAL-ANALYSIS OF THE TURBULENT SHEAR STRESSES FOR DISTORTED SUPERSONIC BOUNDARY-LAYERS, Journal of propulsion and power, 14(1), 1998, pp. 110-118
EXPERIMENTAL INVESTIGATION OF THE FLOW STRUCTURE NEAR A SINGLE WRAPAROUND FIN
Authors: TILMANN CP HUFFMAN RE BUTER TA BOWERSOX RDW
Citation: Cp. Tilmann et al., EXPERIMENTAL INVESTIGATION OF THE FLOW STRUCTURE NEAR A SINGLE WRAPAROUND FIN, Journal of spacecraft and rockets, 34(6), 1997, pp. 729-736
TURBULENT-FLOW STRUCTURE CHARACTERIZATION OF ANGLED INJECTION INTO A SUPERSONIC CROSS-FLOW
Authors: BOWERSOX RDW
Citation: Rdw. Bowersox, TURBULENT-FLOW STRUCTURE CHARACTERIZATION OF ANGLED INJECTION INTO A SUPERSONIC CROSS-FLOW, Journal of spacecraft and rockets, 34(2), 1997, pp. 205-213
PERFORMANCE CHARACTERIZATION OF A HIGHLY OFFSET DIFFUSER WITH VORTEX GENERATOR JETS
Authors: SENSENEY MB BUTER TA BOWERSOX RDW
Citation: Mb. Senseney et al., PERFORMANCE CHARACTERIZATION OF A HIGHLY OFFSET DIFFUSER WITH VORTEX GENERATOR JETS, Journal of propulsion and power, 12(2), 1996, pp. 237-244
EXPERIMENTAL INVESTIGATION OF SUPERSONIC GASEOUS INJECTION INTO A SUPERSONIC FREESTREAM
Authors: MCCANN GJ BOWERSOX RDW
Citation: Gj. Mccann et Rdw. Bowersox, EXPERIMENTAL INVESTIGATION OF SUPERSONIC GASEOUS INJECTION INTO A SUPERSONIC FREESTREAM, AIAA journal, 34(2), 1996, pp. 317-323
TURBULENCE MEASUREMENTS IN A MACH-2.9 BOUNDARY-LAYER INCLUDING MILD PRESSURE-GRADIENTS
Authors: BOWERSOX RDW BUTER TA
Citation: Rdw. Bowersox et Ta. Buter, TURBULENCE MEASUREMENTS IN A MACH-2.9 BOUNDARY-LAYER INCLUDING MILD PRESSURE-GRADIENTS, AIAA journal, 34(12), 1996, pp. 2479-2483
COMBINED LASER-DOPPLER VELOCIMETRY AND CROSS-WIRE ANEMOMETRY ANALYSISFOR SUPERSONIC TURBULENT-FLOW
Authors: BOWERSOX RDW
Citation: Rdw. Bowersox, COMBINED LASER-DOPPLER VELOCIMETRY AND CROSS-WIRE ANEMOMETRY ANALYSISFOR SUPERSONIC TURBULENT-FLOW, AIAA journal, 34(11), 1996, pp. 2269-2275
TECHNIQUE FOR DIRECT MEASUREMENT OF SKIN FRICTION IN HIGH ENTHALPY IMPULSIVE SCRAMJET FLOWFIELDS
Authors: BOWERSOX RDW SCHETZ JA CHADWICK K DEIWERT S
Citation: Rdw. Bowersox et al., TECHNIQUE FOR DIRECT MEASUREMENT OF SKIN FRICTION IN HIGH ENTHALPY IMPULSIVE SCRAMJET FLOWFIELDS, AIAA journal, 33(7), 1995, pp. 1286-1291
MEASUREMENTS OF COMPRESSIBLE TURBULENT-FLOW STRUCTURE IN A SUPERSONICMIXING LAYER
Authors: BOWERSOX RDW SCHETZ JA
Citation: Rdw. Bowersox et Ja. Schetz, MEASUREMENTS OF COMPRESSIBLE TURBULENT-FLOW STRUCTURE IN A SUPERSONICMIXING LAYER, AIAA journal, 33(11), 1995, pp. 2101-2106
MODEL FOR COMPRESSIBLE TURBULENCE IN HYPERSONIC WALL BOUNDARY AND HIGH-SPEED MIXING LAYERS
Authors: BOWERSOX RDW SCHETZ JA
Citation: Rdw. Bowersox et Ja. Schetz, MODEL FOR COMPRESSIBLE TURBULENCE IN HYPERSONIC WALL BOUNDARY AND HIGH-SPEED MIXING LAYERS, AIAA journal, 32(7), 1994, pp. 1531-1533
COMPRESSIBLE TURBULENCE MEASUREMENTS IN A HIGH-SPEED HIGH-REYNOLDS-NUMBER MIXING LAYER
Authors: BOWERSOX RDW SCHETZ JA
Citation: Rdw. Bowersox et Ja. Schetz, COMPRESSIBLE TURBULENCE MEASUREMENTS IN A HIGH-SPEED HIGH-REYNOLDS-NUMBER MIXING LAYER, AIAA journal, 32(4), 1994, pp. 758-764
Risultati: 1-11 |