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Results: 1-17 |
Results: 17
LOAD MEASUREMENTS ON THE LEADING-EDGE EXTENSION, WING, AND BODY OF ANF A-18/
Authors: LEE BHK MARINEAUMES S
Citation: Bhk. Lee et S. Marineaumes, LOAD MEASUREMENTS ON THE LEADING-EDGE EXTENSION, WING, AND BODY OF ANF A-18/, Journal of aircraft, 35(2), 1998, pp. 295-300
NEURAL-NETWORK PARAMETER EXTRACTION WITH APPLICATION TO FLUTTER SIGNALS
Authors: LEE BHK WONG YS
Citation: Bhk. Lee et Ys. Wong, NEURAL-NETWORK PARAMETER EXTRACTION WITH APPLICATION TO FLUTTER SIGNALS, Journal of aircraft, 35(1), 1998, pp. 165-168
ANALYSIS AND COMPUTATION OF NONLINEAR DYNAMIC-RESPONSE OF A 2-DEGREE-OF-FREEDOM SYSTEM AND ITS APPLICATION IN AEROELASTICITY
Authors: LEE BHK GONG L WONG YS
Citation: Bhk. Lee et al., ANALYSIS AND COMPUTATION OF NONLINEAR DYNAMIC-RESPONSE OF A 2-DEGREE-OF-FREEDOM SYSTEM AND ITS APPLICATION IN AEROELASTICITY, Journal of fluids and structures, 11(3), 1997, pp. 225-246
EFFECTS OF STRUCTURAL NONLINEARITIES IN AEROELASTICITY
Authors: LEE BHK GONG L WONG YS
Citation: Bhk. Lee et al., EFFECTS OF STRUCTURAL NONLINEARITIES IN AEROELASTICITY, Nonlinear analysis, 30(5), 1997, pp. 2699-2709
AERODYNAMIC CHARACTERISTICS OF THE F A-18 AT LARGE ROLL ANGLES AND HIGH-INCIDENCE/
Authors: LEE BHK BROWN D
Citation: Bhk. Lee et D. Brown, AERODYNAMIC CHARACTERISTICS OF THE F A-18 AT LARGE ROLL ANGLES AND HIGH-INCIDENCE/, Journal of aircraft, 34(1), 1997, pp. 139-141
INVESTIGATION OF THE UNSTEADY PRESSURE-FLUCTUATIONS ON AN F A-18 WINGAT HIGH-INCIDENCE/
Authors: LEE BHK MARINEAUMES S
Citation: Bhk. Lee et S. Marineaumes, INVESTIGATION OF THE UNSTEADY PRESSURE-FLUCTUATIONS ON AN F A-18 WINGAT HIGH-INCIDENCE/, Journal of aircraft, 33(5), 1996, pp. 888-894
THE AEROELASTIC RESPONSE OF A 2-DIMENSIONAL AIRFOIL WITH BILINEAR ANDCUBIC STRUCTURAL NONLINEARITIES
Authors: PRICE SJ ALIGHANBARI H LEE BHK
Citation: Sj. Price et al., THE AEROELASTIC RESPONSE OF A 2-DIMENSIONAL AIRFOIL WITH BILINEAR ANDCUBIC STRUCTURAL NONLINEARITIES, Journal of fluids and structures, 9(2), 1995, pp. 175-193
CORRELATION OF F A-18 BUFFETING FROM WIND-TUNNEL AND FLIGHT TESTS/
Authors: BEAN DE LEE BHK
Citation: De. Bean et Bhk. Lee, CORRELATION OF F A-18 BUFFETING FROM WIND-TUNNEL AND FLIGHT TESTS/, Journal of aircraft, 32(6), 1995, pp. 1351-1358
NUMERICAL BOUNDARY-CONDITIONS FOR UNSTEADY TRANSONIC FLOW CALCULATIONS
Authors: JIANG H LEE BHK WONG YS
Citation: H. Jiang et al., NUMERICAL BOUNDARY-CONDITIONS FOR UNSTEADY TRANSONIC FLOW CALCULATIONS, International journal for numerical methods in fluids, 18(11), 1994, pp. 1121-1131
POSTINSTABILITY BEHAVIOR OF A 2-DIMENSIONAL AIRFOIL WITH A STRUCTURALNONLINEARITY
Authors: PRICE SJ LEE BHK ALIGHANBARI H
Citation: Sj. Price et al., POSTINSTABILITY BEHAVIOR OF A 2-DIMENSIONAL AIRFOIL WITH A STRUCTURALNONLINEARITY, Journal of aircraft, 31(6), 1994, pp. 1395-1401
VORTICAL FLOW STRUCTURE NEAR THE F A-18 LEX AT HIGH-INCIDENCE/
Authors: LEE BHK VALERIO NR
Citation: Bhk. Lee et Nr. Valerio, VORTICAL FLOW STRUCTURE NEAR THE F A-18 LEX AT HIGH-INCIDENCE/, Journal of aircraft, 31(5), 1994, pp. 1221-1223
STEADY AND UNSTEADY PRESSURE DISTRIBUTIONS ON AN F A-18 WING AT ALPHA=30 DEG/
Authors: LEE BHK VALERIO NR TANG FC
Citation: Bhk. Lee et al., STEADY AND UNSTEADY PRESSURE DISTRIBUTIONS ON AN F A-18 WING AT ALPHA=30 DEG/, Journal of aircraft, 31(4), 1994, pp. 862-867
CHARACTERISTICS OF THE SURFACE PRESSURES ON A F A-18 VERTICAL PIN DUETO BUFFET/
Authors: LEE BHK TANG FC
Citation: Bhk. Lee et Fc. Tang, CHARACTERISTICS OF THE SURFACE PRESSURES ON A F A-18 VERTICAL PIN DUETO BUFFET/, Journal of aircraft, 31(1), 1994, pp. 228-235
ROLE OF KUTTA WAVES ON OSCILLATORY SHOCK MOTION ON AN AIRFOIL
Authors: LEE BHK MURTY H JIANG H
Citation: Bhk. Lee et al., ROLE OF KUTTA WAVES ON OSCILLATORY SHOCK MOTION ON AN AIRFOIL, AIAA journal, 32(4), 1994, pp. 789-796
IMPACT OF ACTIVE CONTROLS TECHNOLOGY ON STRUCTURAL INTEGRITY
Authors: NOLL TE AUSTIN E DONLEY S GRAHAM G HARRIS T KAYNES I LEE BHK SPARROW J
Citation: Te. Noll et al., IMPACT OF ACTIVE CONTROLS TECHNOLOGY ON STRUCTURAL INTEGRITY, Journal of aircraft, 30(6), 1993, pp. 985-992
UNSTEADY PRESSURE AND LOAD MEASUREMENTS ON AN F A-18 VERTICAL FIN/
Authors: LEE BHK TANG FC
Citation: Bhk. Lee et Fc. Tang, UNSTEADY PRESSURE AND LOAD MEASUREMENTS ON AN F A-18 VERTICAL FIN/, Journal of aircraft, 30(5), 1993, pp. 756-762
EVALUATION AND EXTENSION OF THE FLUTTER-MARGIN METHOD FOR FLIGHT FLUTTER PREDICTION
Authors: PRICE SJ LEE BHK
Citation: Sj. Price et Bhk. Lee, EVALUATION AND EXTENSION OF THE FLUTTER-MARGIN METHOD FOR FLIGHT FLUTTER PREDICTION, Journal of aircraft, 30(3), 1993, pp. 395-402
Risultati: 1-17 |