AAAAAA
Results:
1-8
|
Results: 8
Authors:
SCHRECK SJ
FALLER WE
HELIN HE
Citation: Sj. Schreck et al., PITCH RATE AND REYNOLDS-NUMBER EFFECTS ON UNSTEADY BOUNDARY-LAYER-TRANSITION AND SEPARATION, Journal of aircraft, 35(1), 1998, pp. 46-52
Authors:
FALLER WE
SCHRECK SJ
Citation: We. Faller et Sj. Schreck, UNSTEADY FLUID-MECHANICS APPLICATIONS OF NEURAL NETWORKS, Journal of aircraft, 34(1), 1997, pp. 48-55
Authors:
SCHRECK SJ
FALLER WE
LUTTGES MW
Citation: Sj. Schreck et al., DYNAMIC REATTACHMENT ON A DOWNWARD PITCHING FINITE WING, Journal of aircraft, 33(2), 1996, pp. 279-285
Authors:
FALLER WE
SCHRECK SJ
Citation: We. Faller et Sj. Schreck, REAL-TIME PREDICTION OF UNSTEADY AERODYNAMICS - APPLICATION FOR AIRCRAFT CONTROL AND MANEUVERABILITY ENHANCEMENT, IEEE transactions on neural networks, 6(6), 1995, pp. 1461-1468
Authors:
FALLER WE
SCHRECK SJ
HELIN HE
Citation: We. Faller et al., REAL-TIME MODEL OF 3-DIMENSIONAL DYNAMIC REATTACHMENT USING NEURAL NETWORKS, Journal of aircraft, 32(6), 1995, pp. 1177-1182
Authors:
FALLER WE
SCHRECK SJ
LUTTGES MW
Citation: We. Faller et al., NEURAL-NETWORK PREDICTION AND CONTROL OF 3-DIMENSIONAL UNSTEADY SEPARATED FLOWFIELDS, Journal of aircraft, 32(6), 1995, pp. 1213-1220
Authors:
SCHRECK SJ
FALLER WE
LUTTGES MW
Citation: Sj. Schreck et al., NEURAL-NETWORK PREDICTION OF 3-DIMENSIONAL UNSTEADY SEPARATED FLOWFIELDS, Journal of aircraft, 32(1), 1995, pp. 178-185
Authors:
SCHRECK SJ
HELIN HE
Citation: Sj. Schreck et He. Helin, UNSTEADY VORTEX DYNAMICS AND SURFACE PRESSURE TOPOLOGIES ON A FINITE PITCHING WING, Journal of aircraft, 31(4), 1994, pp. 899-907
Risultati:
1-8
|