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Table of contents of journal: *Journal of aircraft (Print)

Results: 1-25/1034

Authors: PARKS EK BACH RE SHIN JH
Citation: Ek. Parks et al., RECONSTRUCTION OF THE 1994 PITTSBURGH AIRPLANE ACCIDENT USING A COMPUTER-SIMULATION, Journal of aircraft, 35(5), 1998, pp. 665-670

Authors: KIM HJ RHO OH
Citation: Hj. Kim et Oh. Rho, AERODYNAMIC DESIGN OF TRANSONIC WINGS USING THE TARGET PRESSURE OPTIMIZATION APPROACH, Journal of aircraft, 35(5), 1998, pp. 671-677

Authors: TANG D DOWELL EH
Citation: D. Tang et Eh. Dowell, UNSTEADY AERODYNAMIC FORCES AND AEROELASTIC RESPONSE FOR EXTERNAL STORE OF AN AIRCRAFT, Journal of aircraft, 35(5), 1998, pp. 678-687

Authors: ANDERSEN G KOLONAY R EASTEP F
Citation: G. Andersen et al., CONTROL-SURFACE REVERSAL IN THE TRANSONIC REGIME, Journal of aircraft, 35(5), 1998, pp. 688-694

Authors: ROBINSON KW LEISHMAN JG
Citation: Kw. Robinson et Jg. Leishman, EFFECTS OF BALLISTIC DAMAGE ON THE AERODYNAMICS OF HELICOPTER ROTOR AIRFOILS, Journal of aircraft, 35(5), 1998, pp. 695-703

Authors: KIM JH RHO OH
Citation: Jh. Kim et Oh. Rho, NUMERICAL-SIMULATION OF FLOWFIELD AROUND AIRFOIL WITH STATIONARY OR OSCILLATING SPOILER, Journal of aircraft, 35(5), 1998, pp. 704-711

Authors: LUPO FM RUSSO GP MAGRI M
Citation: Fm. Lupo et al., SECONDARY CORRECTION FORMULA FOR 2-DIMENSIONAL LIFT COEFFICIENT MEASURED IN A WIND-TUNNEL, Journal of aircraft, 35(5), 1998, pp. 712-719

Authors: RODDEN WP TAYLOR PF MCINTOSH SC
Citation: Wp. Rodden et al., FURTHER REFINEMENT OF THE SUBSONIC DOUBLET-LATTICE METHOD, Journal of aircraft, 35(5), 1998, pp. 720-727

Authors: LOCKARD DP MORRIS PJ
Citation: Dp. Lockard et Pj. Morris, WING-TIP VORTEX CALCULATIONS USING A HIGH-ACCURACY SCHEME, Journal of aircraft, 35(5), 1998, pp. 728-738

Authors: KUO CH HSIEH JK
Citation: Ch. Kuo et Jk. Hsieh, PARALLEL INTERACTION OF INCIDENT VORTEX ARRAY WITH OSCILLATING AIRFOIL, Journal of aircraft, 35(5), 1998, pp. 739-747

Authors: MASSON C VEILLEUX C PARASCHIVOIU I
Citation: C. Masson et al., AIRFOIL WAVE-DRAG PREDICTION USING EULER SOLUTIONS OF TRANSONIC-FLOWS, Journal of aircraft, 35(5), 1998, pp. 748-753

Authors: ISHII T KOBAYASHI H OINUMA H
Citation: T. Ishii et al., MODAL TECHNIQUE FOR ACTIVE CONTROL OF TONES RADIATED FROM A DUCTED FAN, Journal of aircraft, 35(5), 1998, pp. 754-760

Authors: MARQUART JE EASTEP FE
Citation: Je. Marquart et Fe. Eastep, NUMERICAL REPRESENTATION OF PITCHING AND NONPITCHING AIRFOILS UNDERGOING LINEAR ACCELERATION, Journal of aircraft, 35(5), 1998, pp. 761-768

Authors: WARREN ES HASSAN HA
Citation: Es. Warren et Ha. Hassan, TRANSITION CLOSURE-MODEL FOR PREDICTING TRANSITION ONSET, Journal of aircraft, 35(5), 1998, pp. 769-775

Authors: GREENWELL DI
Citation: Di. Greenwell, FREQUENCY-EFFECTS ON DYNAMIC STABILITY DERIVATIVES OBTAINED FROM SMALL-AMPLITUDE OSCILLATORY TESTING, Journal of aircraft, 35(5), 1998, pp. 776-783

Authors: BISHOP JA EASTEP FE STRIZ AG VENKAYYA VB
Citation: Ja. Bishop et al., INFLUENCE OF MODEL COMPLEXITY AND AEROELASTIC CONSTRAINTS ON MULTIDISCIPLINARY OPTIMIZATION OF WINGS, Journal of aircraft, 35(5), 1998, pp. 784-790

Authors: TRACY AL CHOPRA I
Citation: Al. Tracy et I. Chopra, AEROELASTIC STABILITY INVESTIGATION OF A COMPOSITE HINGELESS ROTOR INHOVER, Journal of aircraft, 35(5), 1998, pp. 791-797

Authors: MORTON SA MELVILLE RB VISBAL MR
Citation: Sa. Morton et al., ACCURACY AND COUPLING ISSUES OF AEROELASTIC NAVIER-STOKES SOLUTIONS ON DEFORMING MESHES, Journal of aircraft, 35(5), 1998, pp. 798-805

Authors: BREITSAMTER C LASCHKA B
Citation: C. Breitsamter et B. Laschka, FIN BUFFET PRESSURE EVALUATION BASED ON MEASURED FLOWFIELD VELOCITIES, Journal of aircraft, 35(5), 1998, pp. 806-815

Authors: DONG Y HESS DP
Citation: Y. Dong et Dp. Hess, ACCELERATED VIBRATION LIFE TESTS OF THREADLOCKING ADHESIVE, Journal of aircraft, 35(5), 1998, pp. 816-820

Authors: BRIDGES PD
Citation: Pd. Bridges, AIRCRAFT TIME CONSTANT AND FLYING ON THE STEP, Journal of aircraft, 35(5), 1998, pp. 821-823

Authors: GEORGHIADES GA BANERJEE JR
Citation: Ga. Georghiades et Jr. Banerjee, SIGNIFICANCE OF WASH-OUT ON THE FLUTTER CHARACTERISTICS OF COMPOSITE WINGS, Journal of aircraft, 35(5), 1998, pp. 823-825

Authors: YANG G MORISHITA E
Citation: G. Yang et E. Morishita, PERTURBATION SOLUTION OF DYNAMIC STABILITY DERIVATIVES OVER POINTED BODIES OF REVOLUTION, Journal of aircraft, 35(5), 1998, pp. 825-828

Authors: RAJADAS JN JURY RA CHATTOPADHYAY A
Citation: Jn. Rajadas et al., ENHANCED MULTIOBJECTIVE TECHNIQUE FOR MULTIDISCIPLINARY DESIGN OPTIMIZATION, Journal of aircraft, 35(5), 1998, pp. 828-830

Authors: LIND R FREUDINGER LC VORACEK DF
Citation: R. Lind et al., COMPARISON OF AEROELASTIC EXCITATION MECHANISMS, Journal of aircraft, 35(5), 1998, pp. 830-832
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