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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1973/10/

Folder.. - Mar 05 2025 11:46:26 PM
A Class of Airfoils Designed for High Lift in Incompressible Flow c20031014 [8].pdfA Class of Airfoils Designed for High Lift in Incompressible Flow c20031014 [8].pdf 1030KB Mar 29 2010 09:25:18 AM
Advanced Fighter Controls Flight Simulator for All-Systems Compatibility Testing c20031014 [8].pdfAdvanced Fighter Controls Flight Simulator for All-Systems Compatibility Testing c20031014 [8].pdf 1459KB Mar 29 2010 09:25:18 AM
Blockage Corrections for Large Bluff Bodies near a Wall in a ClosedJet Wind Tunnnel c20031014 [3].pdfBlockage Corrections for Large Bluff Bodies near a Wall in a ClosedJet Wind Tunnnel c20031014 [3].pdf 435KB Mar 29 2010 09:25:18 AM
Buckling of Orthotropic., Curved, Sandwich Panels in Shear and Axial Compression c20031014 [3].pdfBuckling of Orthotropic., Curved, Sandwich Panels in Shear and Axial Compression c20031014 [3].pdf 358KB Mar 29 2010 09:25:18 AM
Comment on ''Simplification of the Wing-Body Problem_ c20031014 [1].pdfComment on ''Simplification of the Wing-Body Problem_ c20031014 [1].pdf 148KB Mar 29 2010 09:25:18 AM
Control System Design Considerations for a Longitudinally Unstable Supersonic Transport c20031014 [8].pdfControl System Design Considerations for a Longitudinally Unstable Supersonic Transport c20031014 [8].pdf 1024KB Mar 29 2010 09:25:18 AM
Development of Sonic Inlets for Turbofan Engines c20031014 [8].pdfDevelopment of Sonic Inlets for Turbofan Engines c20031014 [8].pdf 1335KB Mar 29 2010 09:25:18 AM
Longitudinal Response of an Aircraft due to a Trailing Vortex Pair c20031014 [2].pdfLongitudinal Response of an Aircraft due to a Trailing Vortex Pair c20031014 [2].pdf 238KB Mar 29 2010 09:25:18 AM
Method for Increasing Wind Tunnel Mach Number for Large-Scale Inlet Testing c20031014 [2].pdfMethod for Increasing Wind Tunnel Mach Number for Large-Scale Inlet Testing c20031014 [2].pdf 243KB Mar 29 2010 09:25:18 AM
Prediction of Airfoil Shock Location in Transonic Flow c20031014 [3].pdfPrediction of Airfoil Shock Location in Transonic Flow c20031014 [3].pdf 401KB Mar 29 2010 09:25:18 AM
Prevention of Transition over a Backward Step by Suction c20031014 [5].pdfPrevention of Transition over a Backward Step by Suction c20031014 [5].pdf 688KB Mar 29 2010 09:25:18 AM
Static Aeroelasticity and the Flying Wing c20031014 [9].pdfStatic Aeroelasticity and the Flying Wing c20031014 [9].pdf 1447KB Mar 29 2010 09:25:18 AM