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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1979/9/

Folder.. - Mar 05 2025 11:49:43 PM
Comment on _Flight Test of Stick Force Stability in Attitude-Stabilized Aircraft_ c20030913 [2].pdfComment on _Flight Test of Stick Force Stability in Attitude-Stabilized Aircraft_ c20030913 [2].pdf 313KB Mar 29 2010 10:15:46 AM
Correlation Technique for Ambient Effects on Oxides of Nitrogen c20030913 [6].pdfCorrelation Technique for Ambient Effects on Oxides of Nitrogen c20030913 [6].pdf 565KB Mar 29 2010 10:15:46 AM
Design and Verification of a Turbofan Swirl Augmentor c20030913 [6].pdfDesign and Verification of a Turbofan Swirl Augmentor c20030913 [6].pdf 843KB Mar 29 2010 10:15:46 AM
Drag Reduction by Cooling in Hydrogen-Fueled Aircraft c20030913 [7].pdfDrag Reduction by Cooling in Hydrogen-Fueled Aircraft c20030913 [7].pdf 845KB Mar 29 2010 10:15:46 AM
Effects of Airframe-Inlet Integration on Half -Axisymmetric and Two-Dimensional Supersonic Inlet Performance c20030913 [8].pdfEffects of Airframe-Inlet Integration on Half -Axisymmetric and Two-Dimensional Supersonic Inlet Performance c20030913 [8].pdf 957KB Mar 29 2010 10:15:46 AM
Effects of Dynamic Aeroelasticity on Aircraft Handling Qualities c20030913 [3].pdfEffects of Dynamic Aeroelasticity on Aircraft Handling Qualities c20030913 [3].pdf 425KB Mar 29 2010 10:15:46 AM
High-Altitude Long-Range Sonic Boom Propagation c20030913 [3].pdfHigh-Altitude Long-Range Sonic Boom Propagation c20030913 [3].pdf 456KB Mar 29 2010 10:15:46 AM
Improved Woodward's Panel Method for Calculating Edge Suction Forces c20030913 [4].pdfImproved Woodward's Panel Method for Calculating Edge Suction Forces c20030913 [4].pdf 472KB Mar 29 2010 10:15:46 AM
Integration Time Required to Extract Accurate Data from Transonic Wind-Tunnel Tests c20030913 [6].pdfIntegration Time Required to Extract Accurate Data from Transonic Wind-Tunnel Tests c20030913 [6].pdf 809KB Mar 29 2010 10:15:46 AM
Reply by Authors to W. O. Breuhaus c20030913 [1].pdfReply by Authors to W. O. Breuhaus c20030913 [1].pdf 178KB Mar 29 2010 10:15:46 AM
Subsonic VSTOL Aircraft Configurations with Tandem Wings c20030913 [7].pdfSubsonic VSTOL Aircraft Configurations with Tandem Wings c20030913 [7].pdf 933KB Mar 29 2010 10:15:46 AM
Tilt Nacelle Aerodynamics and Its Application to Fan Blade Stresses c20030913 [8].pdfTilt Nacelle Aerodynamics and Its Application to Fan Blade Stresses c20030913 [8].pdf 1164KB Mar 29 2010 10:15:46 AM
Wake Vortex Measurements of an Ogive Cylinder at CY = 36 Degrees c20030913 [7].pdfWake Vortex Measurements of an Ogive Cylinder at CY = 36 Degrees c20030913 [7].pdf 606KB Mar 29 2010 10:15:46 AM