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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1975/9/

Folder.. - Mar 05 2025 11:47:34 PM
Calculation of vortex sheet roll-up in a rectangular wind tunnel c20040126 [3].pdfCalculation of vortex sheet roll-up in a rectangular wind tunnel c20040126 [3].pdf 356KB Mar 29 2010 10:05:36 AM
Digital Adaptive Model following Flight Control c20040126 [2].pdfDigital Adaptive Model following Flight Control c20040126 [2].pdf 252KB Mar 29 2010 10:05:36 AM
Effect of compression ratio on NOx production by gas turbines c20040126 [2].pdfEffect of compression ratio on NOx production by gas turbines c20040126 [2].pdf 263KB Mar 29 2010 10:05:36 AM
Errata_ Approximate Solution for Minimum Induced Drag of Wings with Given Structural Weight c20040126 [1].pdfErrata_ Approximate Solution for Minimum Induced Drag of Wings with Given Structural Weight c20040126 [1].pdf 113KB Mar 29 2010 10:05:36 AM
Flight Testing the F-12 Series Aircraft c20040126 [4].pdfFlight Testing the F-12 Series Aircraft c20040126 [4].pdf 606KB Mar 29 2010 10:05:36 AM
Multiple slot skin friction reduction c20040126 [2].pdfMultiple slot skin friction reduction c20040126 [2].pdf 293KB Mar 29 2010 10:05:36 AM
Northrop F-5A aircraft transonic buffet pressure data acquisition and response analysis c20040126 [7].pdfNorthrop F-5A aircraft transonic buffet pressure data acquisition and response analysis c20040126 [7].pdf 819KB Mar 29 2010 10:05:36 AM
Predicting Flight by Flight Fatigue Crack Growth Rates c20040126 [7].pdfPredicting Flight by Flight Fatigue Crack Growth Rates c20040126 [7].pdf 1037KB Mar 29 2010 10:05:36 AM
Supercritical Airfoil Flowfield Measurements c20040126 [8].pdfSupercritical Airfoil Flowfield Measurements c20040126 [8].pdf 1403KB Mar 29 2010 10:05:36 AM
Supersonic inlet contour interpolation c20040126 [3].pdfSupersonic inlet contour interpolation c20040126 [3].pdf 404KB Mar 29 2010 10:05:36 AM
Three-Dimensional Wing Jet Interaction Analysis including Jet Distortion Influences c20040126 [8].pdfThree-Dimensional Wing Jet Interaction Analysis including Jet Distortion Influences c20040126 [8].pdf 1102KB Mar 29 2010 10:05:36 AM
Transonic Shock-Free Aerofoil Design by an Analytic Hodograph Method c20040126 [7].pdfTransonic Shock-Free Aerofoil Design by an Analytic Hodograph Method c20040126 [7].pdf 741KB Mar 29 2010 10:05:36 AM
Unsteady Aerodynamics of Slender Delta Wings at Large Angles of Attack c20040126 [9].pdfUnsteady Aerodynamics of Slender Delta Wings at Large Angles of Attack c20040126 [9].pdf 1039KB Mar 29 2010 10:05:36 AM
Vortex Attenuation Obtained in the Langley Vortex Research Facility c20040126 [5].pdfVortex Attenuation Obtained in the Langley Vortex Research Facility c20040126 [5].pdf 1076KB Mar 29 2010 10:05:36 AM