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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1994/1/

Folder.. - Mar 05 2025 11:59:40 PM
Active sound attenuation across a double wall structure c20030718 [5].pdfActive sound attenuation across a double wall structure c20030718 [5].pdf 616KB Mar 27 2010 11:48:10 PM
Aerodynamic design of supersonic cruise wings with a calibrated linearized theory c20030718 [7].pdfAerodynamic design of supersonic cruise wings with a calibrated linearized theory c20030718 [7].pdf 993KB Mar 27 2010 11:48:10 PM
Aerodynamics of airfoils with vortex trapped by two spanwise fences c20030718 [8].pdfAerodynamics of airfoils with vortex trapped by two spanwise fences c20030718 [8].pdf 1166KB Mar 27 2010 11:48:10 PM
Aeronautical activities in Japan (Annual Review for 1992) c20030718 [2].pdfAeronautical activities in Japan (Annual Review for 1992) c20030718 [2].pdf 328KB Mar 27 2010 11:48:10 PM
AIAA Manuscript Review Process c20030718 [1].pdfAIAA Manuscript Review Process c20030718 [1].pdf 150KB Mar 27 2010 11:48:10 PM
Aircraft spoiler effects under wind shear c20030718 [7].pdfAircraft spoiler effects under wind shear c20030718 [7].pdf 711KB Mar 27 2010 11:48:10 PM
Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14 c20030718 [9].pdfApplication of bifurcation theory to the high-angle-of-attack dynamics of the F-14 c20030718 [9].pdf 1175KB Mar 27 2010 11:48:10 PM
Calculations of hot gas ingestion for a STOVL aircraft model c20030724 [7].pdfCalculations of hot gas ingestion for a STOVL aircraft model c20030724 [7].pdf 2205KB Mar 27 2010 11:48:10 PM
Characteristics of the surface pressures on a F A-18 vertical fin due to buffet c20030718 [8].pdfCharacteristics of the surface pressures on a F A-18 vertical fin due to buffet c20030718 [8].pdf 1566KB Mar 27 2010 11:48:10 PM
Computational study of transition front on a swept wing leading-edge model c20030718 [7].pdfComputational study of transition front on a swept wing leading-edge model c20030718 [7].pdf 1037KB Mar 27 2010 11:48:10 PM
Control of cavity flow by upstream mass-injection c20030718 [6].pdfControl of cavity flow by upstream mass-injection c20030718 [6].pdf 826KB Mar 27 2010 11:48:10 PM
Dual-Use and Defense Conversion_ The Aircraft Technology Role c20030718 [1].pdfDual-Use and Defense Conversion_ The Aircraft Technology Role c20030718 [1].pdf 188KB Mar 27 2010 11:48:10 PM
Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty c20030718 [1].pdfEditorial Policy Statement on Numerical Accuracy and Experimental Uncertainty c20030718 [1].pdf 174KB Mar 27 2010 11:48:10 PM
Effect of canard deflection on close-coupled canard-wing-body aerodynamics c20030718 [8].pdfEffect of canard deflection on close-coupled canard-wing-body aerodynamics c20030718 [8].pdf 1097KB Mar 27 2010 11:48:10 PM
Effect of wind-tunnel walls on airfoil droplet impingement c20030718 [6].pdfEffect of wind-tunnel walls on airfoil droplet impingement c20030718 [6].pdf 692KB Mar 27 2010 11:48:10 PM
Ethical Standards for Publication of Aeronautics and Astronautics Research c20030718 [1].pdfEthical Standards for Publication of Aeronautics and Astronautics Research c20030718 [1].pdf 201KB Mar 27 2010 11:48:10 PM
Experimental study of pneumatic control of forebody vortices at high alpha c20030718 [8].pdfExperimental study of pneumatic control of forebody vortices at high alpha c20030718 [8].pdf 1065KB Mar 27 2010 11:48:10 PM
Frequency-domain analysis of fluctuating pressure on a pusher propeller blade surface c20030718 [7].pdfFrequency-domain analysis of fluctuating pressure on a pusher propeller blade surface c20030718 [7].pdf 756KB Mar 27 2010 11:48:10 PM
Fundamentals and similarity transformations of vectored aircraft c20030718 [7].pdfFundamentals and similarity transformations of vectored aircraft c20030718 [7].pdf 961KB Mar 27 2010 11:48:10 PM
Integrated structure control concepts for oblique wing roll control and trim c20030718 [8].pdfIntegrated structure control concepts for oblique wing roll control and trim c20030718 [8].pdf 1114KB Mar 27 2010 11:48:10 PM
Integration of structural optimization in the general design process for aircraft c20030718 [7].pdfIntegration of structural optimization in the general design process for aircraft c20030718 [7].pdf 916KB Mar 27 2010 11:48:10 PM
Investigation of three-dimensional separation at wing body junctions in supersonic flows c20030718 [8].pdfInvestigation of three-dimensional separation at wing body junctions in supersonic flows c20030718 [8].pdf 985KB Mar 27 2010 11:48:10 PM
Measurement of unsteady airloads on an oscillating engine and a wing engine combination c20030718 [6].pdfMeasurement of unsteady airloads on an oscillating engine and a wing engine combination c20030718 [6].pdf 721KB Mar 27 2010 11:48:10 PM
Method for the prediction of wing maximum lift c20030718 [7].pdfMethod for the prediction of wing maximum lift c20030718 [7].pdf 1005KB Mar 27 2010 11:48:10 PM
Multidimensional mount effectiveness for vibration isolation c20030718 [9].pdfMultidimensional mount effectiveness for vibration isolation c20030718 [9].pdf 1083KB Mar 27 2010 11:48:10 PM
Nonlinear response and sonic fatigue of National Aerospace Space Plane surface panels c20030718 [9].pdfNonlinear response and sonic fatigue of National Aerospace Space Plane surface panels c20030718 [9].pdf 1441KB Mar 27 2010 11:48:10 PM
Nonslender waveriders c20030718 [7].pdfNonslender waveriders c20030718 [7].pdf 843KB Mar 27 2010 11:48:10 PM
Panel flutter suppression using adaptive material actuators c20030718 [10].pdfPanel flutter suppression using adaptive material actuators c20030718 [10].pdf 1347KB Mar 27 2010 11:48:10 PM
Remote sensing observations of winter aircraft icing conditions - A case study c20030718 [11].pdfRemote sensing observations of winter aircraft icing conditions - A case study c20030718 [11].pdf 1637KB Mar 27 2010 11:48:10 PM
Reviewers for the Journal of Aircraft-l993_ c20030718 [1].pdfReviewers for the Journal of Aircraft-l993_ c20030718 [1].pdf 116KB Mar 27 2010 11:48:10 PM
Roll moment characteristics of asymmetric tangential leading-edge blowing on a delta wing c20030718 [8].pdfRoll moment characteristics of asymmetric tangential leading-edge blowing on a delta wing c20030718 [8].pdf 955KB Mar 27 2010 11:48:10 PM
Simulation model for tail rotor failure c20030718 [9].pdfSimulation model for tail rotor failure c20030718 [9].pdf 1092KB Mar 27 2010 11:48:10 PM
Sonic boom of the oblique flying wing c20030718 [7].pdfSonic boom of the oblique flying wing c20030718 [7].pdf 912KB Mar 27 2010 11:48:10 PM
Sonic boom predictions using a solution-adaptive full-potential code c20030718 [7].pdfSonic boom predictions using a solution-adaptive full-potential code c20030718 [7].pdf 1008KB Mar 27 2010 11:48:10 PM
Static and dynamic coefficients of a cross-type parachute c20030718 [6].pdfStatic and dynamic coefficients of a cross-type parachute c20030718 [6].pdf 651KB Mar 27 2010 11:48:10 PM
Suppression of flow-induced pressure oscillations in cavities c20030718 [7].pdfSuppression of flow-induced pressure oscillations in cavities c20030718 [7].pdf 908KB Mar 27 2010 11:48:10 PM
The 1994 Team c20030718 [3].pdfThe 1994 Team c20030718 [3].pdf 783KB Mar 27 2010 11:48:10 PM
Unsteady vortex structure over a delta wing c20030718 [6].pdfUnsteady vortex structure over a delta wing c20030718 [6].pdf 1630KB Mar 27 2010 11:48:10 PM
Variable-complexity aerodynamic optimization of a high-speed civil transport wing c20030718 [7].pdfVariable-complexity aerodynamic optimization of a high-speed civil transport wing c20030718 [7].pdf 1103KB Mar 27 2010 11:48:10 PM