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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1998/6/

Folder.. - Mar 06 2025 12:03:01 AM
Aerodynamic Optimization Using Analytic Descriptions of the Design Space c20030724 [9].pdfAerodynamic Optimization Using Analytic Descriptions of the Design Space c20030724 [9].pdf 367KB Mar 27 2010 11:44:12 PM
Altitude Loss in a Split-'S' Maneuver c20030724 [3].pdfAltitude Loss in a Split-'S' Maneuver c20030724 [3].pdf 126KB Mar 27 2010 11:44:12 PM
Approximate Performance of Periodic Hypersonic Cruise Trajectories for Global Reach c20030724 [11].pdfApproximate Performance of Periodic Hypersonic Cruise Trajectories for Global Reach c20030724 [11].pdf 336KB Mar 27 2010 11:44:12 PM
Arbitrary Accuracy Integration Scheme for the Subsonic Doublet Lattice Method c20030724 [3].pdfArbitrary Accuracy Integration Scheme for the Subsonic Doublet Lattice Method c20030724 [3].pdf 131KB Mar 27 2010 11:44:12 PM
Base Drag Reduction Caused by Riblets on a GAW(2) Airfoil c20030724 [4].pdfBase Drag Reduction Caused by Riblets on a GAW(2) Airfoil c20030724 [4].pdf 148KB Mar 27 2010 11:44:12 PM
Behavior of Compression-Loaded Composite Panels with Stringer Terminations and Impact Damage c20030724 [7].pdfBehavior of Compression-Loaded Composite Panels with Stringer Terminations and Impact Damage c20030724 [7].pdf 466KB Mar 27 2010 11:44:12 PM
Certification and Operation of Helicopters in Icing Environments c20030724 [6].pdfCertification and Operation of Helicopters in Icing Environments c20030724 [6].pdf 127KB Mar 27 2010 11:44:12 PM
Characterization of the Flowfield near a Wrap-Around Fin at Mach 2.8 c20030724 [8].pdfCharacterization of the Flowfield near a Wrap-Around Fin at Mach 2.8 c20030724 [8].pdf 1757KB Mar 27 2010 11:44:12 PM
Characterizing the Supercooled Large Droplet Environment with Corresponding Turboprop Aircraft Response c20030724 [9].pdfCharacterizing the Supercooled Large Droplet Environment with Corresponding Turboprop Aircraft Response c20030724 [9].pdf 410KB Mar 27 2010 11:44:12 PM
Comparison of Boundary-Layer Transition Predictions Using Flight Test Data c20030724 [7].pdfComparison of Boundary-Layer Transition Predictions Using Flight Test Data c20030724 [7].pdf 331KB Mar 27 2010 11:44:12 PM
Convergence of the Subsonic Doublet Lattice Method c20030724 [3].pdfConvergence of the Subsonic Doublet Lattice Method c20030724 [3].pdf 134KB Mar 27 2010 11:44:12 PM
Correlation for the Estimation of Afterbody Drag with Hot Jet Exhaust c20030724 [4].pdfCorrelation for the Estimation of Afterbody Drag with Hot Jet Exhaust c20030724 [4].pdf 210KB Mar 27 2010 11:44:12 PM
Development of an Unstructured Mesh Method c20030724 [3].pdfDevelopment of an Unstructured Mesh Method c20030724 [3].pdf 253KB Mar 27 2010 11:44:12 PM
Effect of Fuselage Geometry on Delta-Wing Vortex Breakdown c20030724 [7].pdfEffect of Fuselage Geometry on Delta-Wing Vortex Breakdown c20030724 [7].pdf 423KB Mar 27 2010 11:44:12 PM
Effects of Asymmetric Leading-Edge Flap Deflection on Delta Wings in Roll c20030724 [4].pdfEffects of Asymmetric Leading-Edge Flap Deflection on Delta Wings in Roll c20030724 [4].pdf 182KB Mar 27 2010 11:44:12 PM
Estimation of Aircraft Lateral-Directional Parameters Using Neural Networks c20030724 [6].pdfEstimation of Aircraft Lateral-Directional Parameters Using Neural Networks c20030724 [6].pdf 211KB Mar 27 2010 11:44:12 PM
Flowfield and Acoustic Measurements from a Model Tiltrotor in Hover c20030724 [9].pdfFlowfield and Acoustic Measurements from a Model Tiltrotor in Hover c20030724 [9].pdf 463KB Mar 27 2010 11:44:12 PM
Flutter Control of Wing Boxes Using Piezoelectric Actuators c20030724 [9].pdfFlutter Control of Wing Boxes Using Piezoelectric Actuators c20030724 [9].pdf 288KB Mar 27 2010 11:44:12 PM
Free Vibration of Thick Generally Laminated Quadrilateral Plates Having Arbitrarily Located Point Supports c20030724 [8].pdfFree Vibration of Thick Generally Laminated Quadrilateral Plates Having Arbitrarily Located Point Supports c20030724 [8].pdf 304KB Mar 27 2010 11:44:12 PM
Identifying Aerial Bomb's Aerodynamic Drag Coefficient Curve Using Optimal Dynamic Fitting Method c20030724 [5].pdfIdentifying Aerial Bomb's Aerodynamic Drag Coefficient Curve Using Optimal Dynamic Fitting Method c20030724 [5].pdf 175KB Mar 27 2010 11:44:12 PM
Investigations of High-Speed Civil Transport Inlet Unstart at Angle of Attack c20030724 [6].pdfInvestigations of High-Speed Civil Transport Inlet Unstart at Angle of Attack c20030724 [6].pdf 286KB Mar 27 2010 11:44:12 PM
Lift Enhancement of a Wing Strake Configuration Using Pneumatic Blowing c20030724 [2].pdfLift Enhancement of a Wing Strake Configuration Using Pneumatic Blowing c20030724 [2].pdf 139KB Mar 27 2010 11:44:12 PM
Navier-Stokes Analysis of the Flow About a Flap Edge c20030724 [6].pdfNavier-Stokes Analysis of the Flow About a Flap Edge c20030724 [6].pdf 481KB Mar 27 2010 11:44:12 PM
Neural Network and Regression Approximations in High-Speed Civil Aircraft Design Optimization c20030724 [12].pdfNeural Network and Regression Approximations in High-Speed Civil Aircraft Design Optimization c20030724 [12].pdf 308KB Mar 27 2010 11:44:12 PM
Rapid Prediction of Wing Rock for Slender Delta-Wing Configurations c20030724 [3].pdfRapid Prediction of Wing Rock for Slender Delta-Wing Configurations c20030724 [3].pdf 161KB Mar 27 2010 11:44:12 PM
Two-Dimensional Airfoil Performance Degradation Because of Simulated Freezing Drizzle c20030724 [7].pdfTwo-Dimensional Airfoil Performance Degradation Because of Simulated Freezing Drizzle c20030724 [7].pdf 348KB Mar 27 2010 11:44:12 PM
Wake Forces Implied in the Theodorsen and Goldstein Theories of Propellers c20030724 [6].pdfWake Forces Implied in the Theodorsen and Goldstein Theories of Propellers c20030724 [6].pdf 168KB Mar 27 2010 11:44:12 PM