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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1994/6/

Folder.. - Mar 05 2025 11:59:40 PM
Analysis of a higher harmonic control test to reduce blade vortex interaction noise c20030718 [9].pdfAnalysis of a higher harmonic control test to reduce blade vortex interaction noise c20030718 [9].pdf 1491KB Mar 27 2010 11:49:10 PM
Analytic prediction of lift for delta wings with partial leading-edge thrust c20030718 [4].pdfAnalytic prediction of lift for delta wings with partial leading-edge thrust c20030718 [4].pdf 563KB Mar 27 2010 11:49:10 PM
Author Index c20030718 [2].pdfAuthor Index c20030718 [2].pdf 220KB Mar 27 2010 11:49:10 PM
Chronological Index c20030718 [8].pdfChronological Index c20030718 [8].pdf 1134KB Mar 27 2010 11:49:10 PM
Computational study of plume-induced separation on a hypersonic powered model c20030718 [3].pdfComputational study of plume-induced separation on a hypersonic powered model c20030718 [3].pdf 442KB Mar 27 2010 11:49:10 PM
Computation of the poststall behavior of a circulation controlled airfoil c20030718 [8].pdfComputation of the poststall behavior of a circulation controlled airfoil c20030718 [8].pdf 1085KB Mar 27 2010 11:49:10 PM
Design constraints in the payload-range diagram of ultrahigh capacity transport airplanes c20030718 [5].pdfDesign constraints in the payload-range diagram of ultrahigh capacity transport airplanes c20030718 [5].pdf 646KB Mar 27 2010 11:49:10 PM
Dynamic analysis of bearingless tail rotor blades based on nonlinear shell models c20030718 [9].pdfDynamic analysis of bearingless tail rotor blades based on nonlinear shell models c20030718 [9].pdf 1082KB Mar 27 2010 11:49:10 PM
Effect of leeward flow dividers on the wing rock of a delta wing c20030718 [3].pdfEffect of leeward flow dividers on the wing rock of a delta wing c20030718 [3].pdf 495KB Mar 27 2010 11:49:10 PM
Effect of underwing frost on a transport aircraft airfoil at flight Reynolds number c20030718 [8].pdfEffect of underwing frost on a transport aircraft airfoil at flight Reynolds number c20030718 [8].pdf 1211KB Mar 27 2010 11:49:10 PM
Engineering transition prediction for a hypersonic axisymmetric boundary layer c20030718 [7].pdfEngineering transition prediction for a hypersonic axisymmetric boundary layer c20030718 [7].pdf 788KB Mar 27 2010 11:49:10 PM
Experimental investigation of the flowfield about an unswept afterbody c20030718 [10].pdfExperimental investigation of the flowfield about an unswept afterbody c20030718 [10].pdf 1502KB Mar 27 2010 11:49:10 PM
Experiments on the automatic control of boundary-layer transition c20030718 [3].pdfExperiments on the automatic control of boundary-layer transition c20030718 [3].pdf 387KB Mar 27 2010 11:49:10 PM
Flow study of supersonic wing-nacelle configuration c20030718 [3].pdfFlow study of supersonic wing-nacelle configuration c20030718 [3].pdf 652KB Mar 27 2010 11:49:10 PM
Flow visualization studies on sidewall effects in two-dimensional transonic airfoil testing c20030718 [7].pdfFlow visualization studies on sidewall effects in two-dimensional transonic airfoil testing c20030718 [7].pdf 2147KB Mar 27 2010 11:49:10 PM
Forebody flow control on a full-scale F A-18 aircraft c20030718 [7].pdfForebody flow control on a full-scale F A-18 aircraft c20030718 [7].pdf 1074KB Mar 27 2010 11:49:10 PM
Further analysis of high-rate rolling experiments of a 65-deg delta wing c20030718 [8].pdfFurther analysis of high-rate rolling experiments of a 65-deg delta wing c20030718 [8].pdf 665KB Mar 27 2010 11:49:10 PM
Integration of the supersonic kernel function c20030718 [3].pdfIntegration of the supersonic kernel function c20030718 [3].pdf 456KB Mar 27 2010 11:49:10 PM
Inverse solutions of the Prandtl-Meyer function c20030718 [3].pdfInverse solutions of the Prandtl-Meyer function c20030718 [3].pdf 447KB Mar 27 2010 11:49:10 PM
Limit cycle phenomena in computational transonic aeroelasticity c20030718 [7].pdfLimit cycle phenomena in computational transonic aeroelasticity c20030718 [7].pdf 827KB Mar 27 2010 11:49:10 PM
Method for the prediction of the onset of wing rock c20030718 [3].pdfMethod for the prediction of the onset of wing rock c20030718 [3].pdf 333KB Mar 27 2010 11:49:10 PM
Moving wall effect in relation to other dynamic stall flow mechanisms c20030718 [7].pdfMoving wall effect in relation to other dynamic stall flow mechanisms c20030718 [7].pdf 687KB Mar 27 2010 11:49:10 PM
Navier-Stokes prediction of large-amplitude delta-wing roll oscillations c20030718 [8].pdfNavier-Stokes prediction of large-amplitude delta-wing roll oscillations c20030718 [8].pdf 1025KB Mar 27 2010 11:49:10 PM
Nonlinear angle of twist of advanced composite wing boxes under pure torsion c20030718 [6].pdfNonlinear angle of twist of advanced composite wing boxes under pure torsion c20030718 [6].pdf 824KB Mar 27 2010 11:49:10 PM
Pilot Weather Advisor system c20030718 [4].pdfPilot Weather Advisor system c20030718 [4].pdf 866KB Mar 27 2010 11:49:10 PM
Pneumatic concept for tip-stall control of cranked-arrow wings c20030718 [7].pdfPneumatic concept for tip-stall control of cranked-arrow wings c20030718 [7].pdf 990KB Mar 27 2010 11:49:10 PM
Polar patrol balloon c20030718 [4].pdfPolar patrol balloon c20030718 [4].pdf 559KB Mar 27 2010 11:49:10 PM
Poststability behavior of a two-dimensional airfoil with a structural nonlinearity c20030718 [7].pdfPoststability behavior of a two-dimensional airfoil with a structural nonlinearity c20030718 [7].pdf 880KB Mar 27 2010 11:49:10 PM
Progress in high-lift aerodynamic calculations c20030718 [8].pdfProgress in high-lift aerodynamic calculations c20030718 [8].pdf 1336KB Mar 27 2010 11:49:10 PM
Ram accelerator ballistic range concept for softly accelerating hypersonic free-flying models c20030718 [7].pdfRam accelerator ballistic range concept for softly accelerating hypersonic free-flying models c20030718 [7].pdf 901KB Mar 27 2010 11:49:10 PM
Redundancy in the discrete-vortex method for closed bodies c20030718 [2].pdfRedundancy in the discrete-vortex method for closed bodies c20030718 [2].pdf 282KB Mar 27 2010 11:49:10 PM
Separation control on high-lift airfoils via micro-vortex generators c20030718 [7].pdfSeparation control on high-lift airfoils via micro-vortex generators c20030718 [7].pdf 1030KB Mar 27 2010 11:49:10 PM
Sidewash on the vertical tail in subsonic and supersonic flows c20030718 [5].pdfSidewash on the vertical tail in subsonic and supersonic flows c20030718 [5].pdf 434KB Mar 27 2010 11:49:10 PM
Static aeroelastic characteristics of a composite wing c20030718 [4].pdfStatic aeroelastic characteristics of a composite wing c20030718 [4].pdf 579KB Mar 27 2010 11:49:10 PM
Static pressure distribution in the inlet of a helicopter turbine compressor c20030718 [3].pdfStatic pressure distribution in the inlet of a helicopter turbine compressor c20030718 [3].pdf 376KB Mar 27 2010 11:49:10 PM
Stratospheric towed vehicle concept c20030718 [5].pdfStratospheric towed vehicle concept c20030718 [5].pdf 532KB Mar 27 2010 11:49:10 PM
Structural acoustic calculations in the low-frequency range c20030718 [8].pdfStructural acoustic calculations in the low-frequency range c20030718 [8].pdf 992KB Mar 27 2010 11:49:10 PM
Study of an airfoil with a flap and spoiler c20030718 [4].pdfStudy of an airfoil with a flap and spoiler c20030718 [4].pdf 472KB Mar 27 2010 11:49:10 PM
Subject Index c20030718 [8].pdfSubject Index c20030718 [8].pdf 1058KB Mar 27 2010 11:49:10 PM
Unstructured grid solutions to a wing pylon store configuration c20030718 [6].pdfUnstructured grid solutions to a wing pylon store configuration c20030718 [6].pdf 770KB Mar 27 2010 11:49:10 PM