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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1995/2/

Folder.. - Mar 06 2025 12:01:13 AM
Acoustic spinning-mode analysis by an iterative threshold method c20030718 [8].pdfAcoustic spinning-mode analysis by an iterative threshold method c20030718 [8].pdf 849KB Mar 27 2010 11:47:02 PM
Added mass of high-altitude balloons c20030718 [5].pdfAdded mass of high-altitude balloons c20030718 [5].pdf 573KB Mar 27 2010 11:47:02 PM
Aerodynamic characteristics of vortex flaps on a double-delta planform c20030718 [2].pdfAerodynamic characteristics of vortex flaps on a double-delta planform c20030718 [2].pdf 246KB Mar 27 2010 11:47:02 PM
Aircraft with single-axis aerodynamically deployed wings c20030718 [6].pdfAircraft with single-axis aerodynamically deployed wings c20030718 [6].pdf 700KB Mar 27 2010 11:47:02 PM
Analysis of vortex bursting utilizing three-dimensional laser measurements c20030718 [10].pdfAnalysis of vortex bursting utilizing three-dimensional laser measurements c20030718 [10].pdf 1233KB Mar 27 2010 11:47:02 PM
Applicability of Newtonian and linear theory to slender hypersonic bodies c20030718 [4].pdfApplicability of Newtonian and linear theory to slender hypersonic bodies c20030718 [4].pdf 524KB Mar 27 2010 11:47:02 PM
Case for aircraft with outboard horizontal stabilizers c20030718 [6].pdfCase for aircraft with outboard horizontal stabilizers c20030718 [6].pdf 1097KB Mar 27 2010 11:47:02 PM
CFD-based aerodynamic approximation concepts optimization of a two-dimensional scramjet vehicle c20030718 [8].pdfCFD-based aerodynamic approximation concepts optimization of a two-dimensional scramjet vehicle c20030718 [8].pdf 1161KB Mar 27 2010 11:47:02 PM
Comment on _Physics of Coanda Jet Detachment at High-pressure Ratio_ c20030718 [1].pdfComment on _Physics of Coanda Jet Detachment at High-pressure Ratio_ c20030718 [1].pdf 61KB Mar 27 2010 11:47:02 PM
Computation of passively controlled transonic wing c20030718 [6].pdfComputation of passively controlled transonic wing c20030718 [6].pdf 682KB Mar 27 2010 11:47:02 PM
Concurrent engineering in design of aircraft structures c20030718 [8].pdfConcurrent engineering in design of aircraft structures c20030718 [8].pdf 1120KB Mar 27 2010 11:47:02 PM
Directional stability of a large receiver aircraft in air-to-air refueling c20030718 [3].pdfDirectional stability of a large receiver aircraft in air-to-air refueling c20030718 [3].pdf 442KB Mar 27 2010 11:47:02 PM
Effect of geometry and mass distribution on tumbling characteristics of flying wings c20030718 [7].pdfEffect of geometry and mass distribution on tumbling characteristics of flying wings c20030718 [7].pdf 966KB Mar 27 2010 11:47:02 PM
Evolution of airplane gust loads design requirements c20030718 [12].pdfEvolution of airplane gust loads design requirements c20030718 [12].pdf 1896KB Mar 27 2010 11:47:02 PM
Finite state induced flow models. I - Two-dimensional thin airfoil c20030718 [10].pdfFinite state induced flow models. I - Two-dimensional thin airfoil c20030718 [10].pdf 960KB Mar 27 2010 11:47:02 PM
Finite state induced flow models. II - Three-dimensional rotor disk c20030718 [11].pdfFinite state induced flow models. II - Three-dimensional rotor disk c20030718 [11].pdf 1192KB Mar 27 2010 11:47:02 PM
Global nonlinear aerodynamic modeling using multivariate orthogonal functions c20030718 [8].pdfGlobal nonlinear aerodynamic modeling using multivariate orthogonal functions c20030718 [8].pdf 1123KB Mar 27 2010 11:47:02 PM
Hypersonic inviscid and viscous flow over a wedge and cone c20030718 [7].pdfHypersonic inviscid and viscous flow over a wedge and cone c20030718 [7].pdf 645KB Mar 27 2010 11:47:02 PM
Ice accretion on aircraft wings with thermodynamic effects c20030718 [3].pdfIce accretion on aircraft wings with thermodynamic effects c20030718 [3].pdf 423KB Mar 27 2010 11:47:02 PM
Impact of aeroelastic-propulsive interactions on flight dynamics of a hypersonic vehicle c20030718 [8].pdfImpact of aeroelastic-propulsive interactions on flight dynamics of a hypersonic vehicle c20030718 [8].pdf 1070KB Mar 27 2010 11:47:02 PM
Influence of sideslip on double delta wing aerodynamics c20030718 [3].pdfInfluence of sideslip on double delta wing aerodynamics c20030718 [3].pdf 436KB Mar 27 2010 11:47:02 PM
Interpretation of experimental high-alpha aerodynamics - Implications for flight prediction c20030718 [15].pdfInterpretation of experimental high-alpha aerodynamics - Implications for flight prediction c20030718 [15].pdf 2518KB Mar 27 2010 11:47:02 PM
Multidisciplinary design integration methodology for a supersonic transport aircraft c20030718 [7].pdfMultidisciplinary design integration methodology for a supersonic transport aircraft c20030718 [7].pdf 952KB Mar 27 2010 11:47:02 PM
Multidisciplinary optimization in aircraft design using analytic technology models c20030718 [8].pdfMultidisciplinary optimization in aircraft design using analytic technology models c20030718 [8].pdf 896KB Mar 27 2010 11:47:02 PM
Multiple order pole pure lag rational function approximations for unsteady aerodynamics c20030718 [9].pdfMultiple order pole pure lag rational function approximations for unsteady aerodynamics c20030718 [9].pdf 1084KB Mar 27 2010 11:47:02 PM
Navier-Stokes solutions for an oscillating double-delta wing c20030718 [7].pdfNavier-Stokes solutions for an oscillating double-delta wing c20030718 [7].pdf 1515KB Mar 27 2010 11:47:02 PM
Numerical simulation of the jet produced by an internal aircraft explosion c20030718 [7].pdfNumerical simulation of the jet produced by an internal aircraft explosion c20030718 [7].pdf 1653KB Mar 27 2010 11:47:02 PM
Numerical study of a supersonic open cavity flow and pressure oscillation control c20030718 [7].pdfNumerical study of a supersonic open cavity flow and pressure oscillation control c20030718 [7].pdf 912KB Mar 27 2010 11:47:02 PM
Possible 'impossible' turn c20030718 [6].pdfPossible 'impossible' turn c20030718 [6].pdf 721KB Mar 27 2010 11:47:02 PM
Pressure-Sensitive Paint Measurements on a Supersonic High-Sweep Oblique Wing Model c20030718 [11].pdfPressure-Sensitive Paint Measurements on a Supersonic High-Sweep Oblique Wing Model c20030718 [11].pdf 3528KB Mar 27 2010 11:47:02 PM
Robust and efficient trimming algorithm for application to advanced mathematical models of rotorcraft c20030718 [4].pdfRobust and efficient trimming algorithm for application to advanced mathematical models of rotorcraft c20030718 [4].pdf 521KB Mar 27 2010 11:47:02 PM
When in-flight simulation is necessary c20030718 [5].pdfWhen in-flight simulation is necessary c20030718 [5].pdf 1072KB Mar 27 2010 11:47:02 PM
Wind-tunnel measurements of hazard posed by lift-generated wakes c20030718 [7].pdfWind-tunnel measurements of hazard posed by lift-generated wakes c20030718 [7].pdf 819KB Mar 27 2010 11:47:02 PM
Wing flutter boundary prediction using unsteady Euler aerodynamic method c20030718 [7].pdfWing flutter boundary prediction using unsteady Euler aerodynamic method c20030718 [7].pdf 1153KB Mar 27 2010 11:47:02 PM
Wing leading-edge design concepts for airbreathing hypersonic waveriders c20030718 [6].pdfWing leading-edge design concepts for airbreathing hypersonic waveriders c20030718 [6].pdf 817KB Mar 27 2010 11:47:02 PM