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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1995/5/

Folder.. - Mar 06 2025 12:01:13 AM
Acoustics of a counter-rotating shrouded propfan - Prediction and data c20030728 [8].pdfAcoustics of a counter-rotating shrouded propfan - Prediction and data c20030728 [8].pdf 1053KB Mar 27 2010 11:47:42 PM
Aerodynamics and acoustics of rotor blade-vortex interactions c20030728 [8].pdfAerodynamics and acoustics of rotor blade-vortex interactions c20030728 [8].pdf 869KB Mar 27 2010 11:47:42 PM
Aeroelastic actuation using elastic and induced strain anisotropy c20030728 [8].pdfAeroelastic actuation using elastic and induced strain anisotropy c20030728 [8].pdf 1062KB Mar 27 2010 11:47:42 PM
Analysis of rolled delta wing flows using effective sweep and attack angles c20030728 [7].pdfAnalysis of rolled delta wing flows using effective sweep and attack angles c20030728 [7].pdf 1077KB Mar 27 2010 11:47:42 PM
Analysis of tangential slot blowing on F A-18 isolated forebody c20030728 [7].pdfAnalysis of tangential slot blowing on F A-18 isolated forebody c20030728 [7].pdf 905KB Mar 27 2010 11:47:42 PM
Analytic sensitivity and approximation of skin buckling constraints in wing-shape synthesis c20030728 [12].pdfAnalytic sensitivity and approximation of skin buckling constraints in wing-shape synthesis c20030728 [12].pdf 1453KB Mar 27 2010 11:47:42 PM
Application of an artificial neural network as a flight test data estimator c20030728 [7].pdfApplication of an artificial neural network as a flight test data estimator c20030728 [7].pdf 962KB Mar 27 2010 11:47:42 PM
Asymptotic expression of the forces induced by a strong jet in a crossflow c20030728 [3].pdfAsymptotic expression of the forces induced by a strong jet in a crossflow c20030728 [3].pdf 444KB Mar 27 2010 11:47:42 PM
Co- and contrarotating streamwise vortices in a turbulent boundary layer c20030728 [7].pdfCo- and contrarotating streamwise vortices in a turbulent boundary layer c20030728 [7].pdf 870KB Mar 27 2010 11:47:42 PM
Comment on 'Inverse solutions of the Prandtl-Meyer function' c20030728 [1].pdfComment on 'Inverse solutions of the Prandtl-Meyer function' c20030728 [1].pdf 94KB Mar 27 2010 11:47:42 PM
Compressibility effects on vortex breakdown onset above a 75-degree sweep delta wing c20030718 [7].pdfCompressibility effects on vortex breakdown onset above a 75-degree sweep delta wing c20030718 [7].pdf 908KB Mar 27 2010 11:47:42 PM
De-Dopplerization of aircraft acoustic signals c20030728 [6].pdfDe-Dopplerization of aircraft acoustic signals c20030728 [6].pdf 675KB Mar 27 2010 11:47:42 PM
Decomposition-based optimization procedure for high-speed prop-rotors using composite tailoring c20030728 [8].pdfDecomposition-based optimization procedure for high-speed prop-rotors using composite tailoring c20030728 [8].pdf 1080KB Mar 27 2010 11:47:42 PM
Development of transonic area-rule methodology c20030728 [6].pdfDevelopment of transonic area-rule methodology c20030728 [6].pdf 769KB Mar 27 2010 11:47:42 PM
Effect of blade-tip planform on shock wave of advancing helicopter blade c20030718 [7].pdfEffect of blade-tip planform on shock wave of advancing helicopter blade c20030718 [7].pdf 708KB Mar 27 2010 11:47:42 PM
Effect of canard oscillations on an X-31A-like model in pitching maneuver c20030728 [4].pdfEffect of canard oscillations on an X-31A-like model in pitching maneuver c20030728 [4].pdf 493KB Mar 27 2010 11:47:42 PM
Effect of delta planform tip sail incidence and arrangement on wing performance c20030728 [3].pdfEffect of delta planform tip sail incidence and arrangement on wing performance c20030728 [3].pdf 385KB Mar 27 2010 11:47:42 PM
Effects of large blockage in wind-tunnel testing c20030728 [4].pdfEffects of large blockage in wind-tunnel testing c20030728 [4].pdf 587KB Mar 27 2010 11:47:42 PM
Effects of strakes on a glancing shock wave turbulent boundary-layer interaction c20030728 [8].pdfEffects of strakes on a glancing shock wave turbulent boundary-layer interaction c20030728 [8].pdf 1266KB Mar 27 2010 11:47:42 PM
Equilibrium of bolted joints subjected to in-plane external loading c20030728 [6].pdfEquilibrium of bolted joints subjected to in-plane external loading c20030728 [6].pdf 646KB Mar 27 2010 11:47:42 PM
Evaluation of blockage interference on propellers in a perforated-wall wind tunnel c20030728 [9].pdfEvaluation of blockage interference on propellers in a perforated-wall wind tunnel c20030728 [9].pdf 944KB Mar 27 2010 11:47:42 PM
Experimental and analytical investigation of transonic limit-cycle oscillations of a flaperon c20030718 [6].pdfExperimental and analytical investigation of transonic limit-cycle oscillations of a flaperon c20030718 [6].pdf 708KB Mar 27 2010 11:47:42 PM
Experimental investigation of three-dimensional dynamic stall model oscillating in pitch c20030728 [10].pdfExperimental investigation of three-dimensional dynamic stall model oscillating in pitch c20030728 [10].pdf 1189KB Mar 27 2010 11:47:42 PM
Experimental study of lift-enhancing tabs on a two-element airfoil c20030728 [7].pdfExperimental study of lift-enhancing tabs on a two-element airfoil c20030728 [7].pdf 880KB Mar 27 2010 11:47:42 PM
Inverse method for airfoil design c20030728 [11].pdfInverse method for airfoil design c20030728 [11].pdf 1139KB Mar 27 2010 11:47:42 PM
Matched-filter and stochastic-simulation-based methods of gust loads prediction c20030728 [9].pdfMatched-filter and stochastic-simulation-based methods of gust loads prediction c20030728 [9].pdf 966KB Mar 27 2010 11:47:42 PM
Momentum, pressure, and energy in the Trefftz-plane c20030718 [12].pdfMomentum, pressure, and energy in the Trefftz-plane c20030718 [12].pdf 1611KB Mar 27 2010 11:47:42 PM
Origin of computed unsteadiness in the shear layer of delta wings c20030728 [3].pdfOrigin of computed unsteadiness in the shear layer of delta wings c20030728 [3].pdf 724KB Mar 27 2010 11:47:42 PM
Oscillatory behavior of helicopter rotor airloads in the blade stall regime c20030728 [2].pdfOscillatory behavior of helicopter rotor airloads in the blade stall regime c20030728 [2].pdf 293KB Mar 27 2010 11:47:42 PM
Pitch rate and pitch-axis location effects on vortex breakdown onset c20030718 [7].pdfPitch rate and pitch-axis location effects on vortex breakdown onset c20030718 [7].pdf 821KB Mar 27 2010 11:47:42 PM
Reply by the Authors to G. Emanuel c20030728 [1].pdfReply by the Authors to G. Emanuel c20030728 [1].pdf 92KB Mar 27 2010 11:47:42 PM
Rotor aerodynamic loads computation using a constant vorticity contour free wake model c20030718 [10].pdfRotor aerodynamic loads computation using a constant vorticity contour free wake model c20030718 [10].pdf 1266KB Mar 27 2010 11:47:42 PM
Structural modeling for optimization of low aspect ratio composite wings c20030728 [10].pdfStructural modeling for optimization of low aspect ratio composite wings c20030728 [10].pdf 1134KB Mar 27 2010 11:47:42 PM
Study of the pressure distribution on an aircraft tire-wheel interface c20030718 [8].pdfStudy of the pressure distribution on an aircraft tire-wheel interface c20030718 [8].pdf 1231KB Mar 27 2010 11:47:42 PM
Unstructured Euler flutter analysis of two-dimensional wing-tail configuration c20030728 [4].pdfUnstructured Euler flutter analysis of two-dimensional wing-tail configuration c20030728 [4].pdf 540KB Mar 27 2010 11:47:42 PM
Viscous flow past a nacelle in proximity to a flat plate c20030728 [3].pdfViscous flow past a nacelle in proximity to a flat plate c20030728 [3].pdf 407KB Mar 27 2010 11:47:42 PM
Visualization of choked supersonic flow-through engine nacelles c20030728 [3].pdfVisualization of choked supersonic flow-through engine nacelles c20030728 [3].pdf 808KB Mar 27 2010 11:47:42 PM
Vortex-in-cell analysis of wing wake roll-up c20030718 [8].pdfVortex-in-cell analysis of wing wake roll-up c20030718 [8].pdf 977KB Mar 27 2010 11:47:42 PM
Vortex asymmetry and induced side forces on elliptic cones at high incidence c20030728 [8].pdfVortex asymmetry and induced side forces on elliptic cones at high incidence c20030728 [8].pdf 930KB Mar 27 2010 11:47:42 PM
Wake integration to predict wing span loading from a numerical simulation c20030728 [3].pdfWake integration to predict wing span loading from a numerical simulation c20030728 [3].pdf 345KB Mar 27 2010 11:47:42 PM
Wall temperature effects on the stability of laminar boundary layers c20030728 [3].pdfWall temperature effects on the stability of laminar boundary layers c20030728 [3].pdf 368KB Mar 27 2010 11:47:42 PM
Wedge-cone waverider configuration for engine-airframe interaction c20030728 [3].pdfWedge-cone waverider configuration for engine-airframe interaction c20030728 [3].pdf 511KB Mar 27 2010 11:47:42 PM
Wing performance in moderate rain c20030728 [6].pdfWing performance in moderate rain c20030728 [6].pdf 1277KB Mar 27 2010 11:47:42 PM