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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1994/4/

Folder.. - Mar 05 2025 11:59:40 PM
Aircraft thrust vectoring using flexible nonaxisymmetric nozzles c20030718 [3].pdfAircraft thrust vectoring using flexible nonaxisymmetric nozzles c20030718 [3].pdf 486KB Mar 27 2010 11:48:44 PM
Airfoil shaping for reduced radar cross section c20030718 [7].pdfAirfoil shaping for reduced radar cross section c20030718 [7].pdf 826KB Mar 27 2010 11:48:44 PM
Analytic sensitivities for shape optimization in equivalent plate structural wing models c20030718 [9].pdfAnalytic sensitivities for shape optimization in equivalent plate structural wing models c20030718 [9].pdf 1053KB Mar 27 2010 11:48:44 PM
Comment on 'Effect of fuselage on delta wing vortex breakdown' c20030718 [2].pdfComment on 'Effect of fuselage on delta wing vortex breakdown' c20030718 [2].pdf 272KB Mar 27 2010 11:48:44 PM
Comment on 'Model flight tests and neutral point determination' c20030718 [2].pdfComment on 'Model flight tests and neutral point determination' c20030718 [2].pdf 217KB Mar 27 2010 11:48:44 PM
Comparing aircraft agility using Mahalanobis distances c20030718 [2].pdfComparing aircraft agility using Mahalanobis distances c20030718 [2].pdf 294KB Mar 27 2010 11:48:44 PM
Direct solution of the aeroelastic stability equations c20030718 [3].pdfDirect solution of the aeroelastic stability equations c20030718 [3].pdf 388KB Mar 27 2010 11:48:44 PM
Doubled-point method for supersonic unsteady aerodynamics of nonplanar lifting surfaces c20030718 [8].pdfDoubled-point method for supersonic unsteady aerodynamics of nonplanar lifting surfaces c20030718 [8].pdf 865KB Mar 27 2010 11:48:44 PM
Effect of a fuselage on delta wing vortex breakdown c20030718 [4].pdfEffect of a fuselage on delta wing vortex breakdown c20030718 [4].pdf 760KB Mar 27 2010 11:48:44 PM
Effect of sidewall boundary layer on transonic flow over a wing c20030718 [3].pdfEffect of sidewall boundary layer on transonic flow over a wing c20030718 [3].pdf 447KB Mar 27 2010 11:48:44 PM
Experimental investigation of rotor lifting surface interactions c20030718 [9].pdfExperimental investigation of rotor lifting surface interactions c20030718 [9].pdf 1213KB Mar 27 2010 11:48:44 PM
Experimental investigation of vortex breakdown over a sideslipping canard-configured aircraft model c20030718 [4].pdfExperimental investigation of vortex breakdown over a sideslipping canard-configured aircraft model c20030718 [4].pdf 760KB Mar 27 2010 11:48:44 PM
Experimental investigation of vortex flaps on thick delta wings c20030718 [4].pdfExperimental investigation of vortex flaps on thick delta wings c20030718 [4].pdf 593KB Mar 27 2010 11:48:44 PM
Flight loads test of the indigenous defensive fighter c20030718 [7].pdfFlight loads test of the indigenous defensive fighter c20030718 [7].pdf 731KB Mar 27 2010 11:48:44 PM
Flowfield study of a close-coupled canard configuration c20030718 [7].pdfFlowfield study of a close-coupled canard configuration c20030718 [7].pdf 1439KB Mar 27 2010 11:48:44 PM
Forebody tangential slot blowing on an aircraft geometry c20030718 [7].pdfForebody tangential slot blowing on an aircraft geometry c20030718 [7].pdf 963KB Mar 27 2010 11:48:44 PM
Helicopter rotor lift distributions for minimum-induced power loss c20030718 [9].pdfHelicopter rotor lift distributions for minimum-induced power loss c20030718 [9].pdf 1215KB Mar 27 2010 11:48:44 PM
Hover acoustic characteristics of the XV-15 with advanced technology blades c20030718 [8].pdfHover acoustic characteristics of the XV-15 with advanced technology blades c20030718 [8].pdf 2272KB Mar 27 2010 11:48:44 PM
Identification of helicopter component loads using multiple regression c20030718 [7].pdfIdentification of helicopter component loads using multiple regression c20030718 [7].pdf 809KB Mar 27 2010 11:48:44 PM
Interrupted jet as a candidate for mixing enhancement in aircraft ejectors c20030718 [7].pdfInterrupted jet as a candidate for mixing enhancement in aircraft ejectors c20030718 [7].pdf 894KB Mar 27 2010 11:48:44 PM
Jet ground vortex formation by annular jets c20030718 [8].pdfJet ground vortex formation by annular jets c20030718 [8].pdf 1086KB Mar 27 2010 11:48:44 PM
Lessons from application of equivalent plate structural molding to an HSCT wing c20030718 [8].pdfLessons from application of equivalent plate structural molding to an HSCT wing c20030718 [8].pdf 949KB Mar 27 2010 11:48:44 PM
Locally interactive laminar separation bubble mode c20030718 [9].pdfLocally interactive laminar separation bubble mode c20030718 [9].pdf 1274KB Mar 27 2010 11:48:44 PM
Low-speed characteristics for the wing-canard configuration of the International Vortex Flow Experiment c20030718 [11].pdfLow-speed characteristics for the wing-canard configuration of the International Vortex Flow Experiment c20030718 [11].pdf 1521KB Mar 27 2010 11:48:44 PM
Nonlinear flutter analysis of wings at high angle of attack c20030718 [2].pdfNonlinear flutter analysis of wings at high angle of attack c20030718 [2].pdf 268KB Mar 27 2010 11:48:44 PM
Numerical method for estimation of propeller efficiencies c20030718 [3].pdfNumerical method for estimation of propeller efficiencies c20030718 [3].pdf 477KB Mar 27 2010 11:48:44 PM
Parametric studies of bearing strength for fiber metal laminates c20030718 [10].pdfParametric studies of bearing strength for fiber metal laminates c20030718 [10].pdf 1777KB Mar 27 2010 11:48:44 PM
Pilot evaluations of augmented flight simulator motion c20030718 [5].pdfPilot evaluations of augmented flight simulator motion c20030718 [5].pdf 634KB Mar 27 2010 11:48:44 PM
Prediction of ice accretion with viscous effects on aircraft wings c20030718 [7].pdfPrediction of ice accretion with viscous effects on aircraft wings c20030718 [7].pdf 885KB Mar 27 2010 11:48:44 PM
Prevention of jump in inertia-coupled roll maneuvers of aircraft c20030718 [3].pdfPrevention of jump in inertia-coupled roll maneuvers of aircraft c20030718 [3].pdf 403KB Mar 27 2010 11:48:44 PM
Problem of dynamic stall simulation revisited c20030718 [5].pdfProblem of dynamic stall simulation revisited c20030718 [5].pdf 552KB Mar 27 2010 11:48:44 PM
Quantitative study of unsteady compressible flow on an oscillating airfoil c20030718 [7].pdfQuantitative study of unsteady compressible flow on an oscillating airfoil c20030718 [7].pdf 2190KB Mar 27 2010 11:48:44 PM
Separation bubble model for low Reynolds number airfoil applications c20030718 [6].pdfSeparation bubble model for low Reynolds number airfoil applications c20030718 [6].pdf 765KB Mar 27 2010 11:48:44 PM
Several considerations regarding the variable blade length rotor c20030718 [3].pdfSeveral considerations regarding the variable blade length rotor c20030718 [3].pdf 493KB Mar 27 2010 11:48:44 PM
Severe turbulence and maneuvering from airline flight records c20030718 [8].pdfSevere turbulence and maneuvering from airline flight records c20030718 [8].pdf 910KB Mar 27 2010 11:48:44 PM
Side-force control on a diamond forebody at high angles of attack c20030718 [7].pdfSide-force control on a diamond forebody at high angles of attack c20030718 [7].pdf 879KB Mar 27 2010 11:48:44 PM
Side force augmentation at high angle of attack from pneumatic vortex control c20030718 [8].pdfSide force augmentation at high angle of attack from pneumatic vortex control c20030718 [8].pdf 917KB Mar 27 2010 11:48:44 PM
Simple equations for helical vortex wakes c20030718 [2].pdfSimple equations for helical vortex wakes c20030718 [2].pdf 288KB Mar 27 2010 11:48:44 PM
Steady and unsteady pressure distributions on an F A-18 wing at alpha = 30 deg c20030718 [6].pdfSteady and unsteady pressure distributions on an F A-18 wing at alpha = 30 deg c20030718 [6].pdf 1048KB Mar 27 2010 11:48:44 PM
Study of dynamic stall using real-time interferometry c20030718 [4].pdfStudy of dynamic stall using real-time interferometry c20030718 [4].pdf 1076KB Mar 27 2010 11:48:44 PM
Subsonic state and dynamic stability characteristics of a NASP configuration c20030718 [7].pdfSubsonic state and dynamic stability characteristics of a NASP configuration c20030718 [7].pdf 821KB Mar 27 2010 11:48:44 PM
Tailoring stall characteristics using leading edge droop modification c20030718 [6].pdfTailoring stall characteristics using leading edge droop modification c20030718 [6].pdf 817KB Mar 27 2010 11:48:44 PM
Time-accurate computational fluid dynamics approach to transonic store separation trajectory prediction c20030718 [6].pdfTime-accurate computational fluid dynamics approach to transonic store separation trajectory prediction c20030718 [6].pdf 915KB Mar 27 2010 11:48:44 PM
Tree lookahead in air combat c20030718 [4].pdfTree lookahead in air combat c20030718 [4].pdf 549KB Mar 27 2010 11:48:44 PM
Turbulence evaluation for use with supercritical airfoils c20030718 [3].pdfTurbulence evaluation for use with supercritical airfoils c20030718 [3].pdf 448KB Mar 27 2010 11:48:44 PM
Turbulent flow structure associated with vortex-induced fin buffeting c20030718 [9].pdfTurbulent flow structure associated with vortex-induced fin buffeting c20030718 [9].pdf 1181KB Mar 27 2010 11:48:44 PM
Unsteady vortex dynamics and surface pressure topologies on a finite pitching wing c20030718 [9].pdfUnsteady vortex dynamics and surface pressure topologies on a finite pitching wing c20030718 [9].pdf 1650KB Mar 27 2010 11:48:44 PM
Use of artificial neural networks for buffet environments c20030718 [6].pdfUse of artificial neural networks for buffet environments c20030718 [6].pdf 910KB Mar 27 2010 11:48:44 PM