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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1972/9/

Folder.. - Mar 05 2025 11:45:57 PM
Adaptive Model Following Systems for Flight Control and Simulation c20031012 [7].pdfAdaptive Model Following Systems for Flight Control and Simulation c20031012 [7].pdf 759KB Mar 29 2010 09:22:52 AM
Aeroelastic Optimization of a Panel in High Mach Number Supersonic Flow c20031012 [7].pdfAeroelastic Optimization of a Panel in High Mach Number Supersonic Flow c20031012 [7].pdf 857KB Mar 29 2010 09:22:52 AM
Analysis and Correlation of Data on Pressure Fluctuations in Separated Flow c20031012 [4].pdfAnalysis and Correlation of Data on Pressure Fluctuations in Separated Flow c20031012 [4].pdf 690KB Mar 29 2010 09:22:52 AM
Analytical Method for Combining the Interaction of Inlet Distortion and Turbulence c20031012 [6].pdfAnalytical Method for Combining the Interaction of Inlet Distortion and Turbulence c20031012 [6].pdf 816KB Mar 29 2010 09:22:52 AM
An Improved Solution of the Two-Dimensional Jet-Flapped Airfoil Problem c20031017 [5].pdfAn Improved Solution of the Two-Dimensional Jet-Flapped Airfoil Problem c20031017 [5].pdf 685KB Mar 29 2010 09:22:52 AM
Application of Thermal Barriers to High-Temperature Engine Components c20031012 [2].pdfApplication of Thermal Barriers to High-Temperature Engine Components c20031012 [2].pdf 305KB Mar 29 2010 09:22:52 AM
A Stability Analysis for Tethered Aerodynamically Shaped Balloons c20031012 [6].pdfA Stability Analysis for Tethered Aerodynamically Shaped Balloons c20031012 [6].pdf 769KB Mar 29 2010 09:22:52 AM
Calculation of Separation Points in Incompressible Turbulent Flows c20031012 [7].pdfCalculation of Separation Points in Incompressible Turbulent Flows c20031012 [7].pdf 937KB Mar 29 2010 09:22:52 AM
Comment on _ Convergence Proof of Discrete-Panel Wing Loading Theories_ c20031012 [3].pdfComment on _ Convergence Proof of Discrete-Panel Wing Loading Theories_ c20031012 [3].pdf 386KB Mar 29 2010 09:22:52 AM
Development of the F-15 Integrated Data System c20031012 [6].pdfDevelopment of the F-15 Integrated Data System c20031012 [6].pdf 927KB Mar 29 2010 09:22:52 AM
Effect of Air Injection on the Torque Produced by a Trailing Vortex c20031012 [3].pdfEffect of Air Injection on the Torque Produced by a Trailing Vortex c20031012 [3].pdf 513KB Mar 29 2010 09:22:52 AM
Effect of Several Wing Tip Modifications on a Trailing Vortex c20031012 [3].pdfEffect of Several Wing Tip Modifications on a Trailing Vortex c20031012 [3].pdf 416KB Mar 29 2010 09:22:52 AM
Forward-Speed Effects on Peripheral-Jet Ground Support Systems c20031012 [7].pdfForward-Speed Effects on Peripheral-Jet Ground Support Systems c20031012 [7].pdf 959KB Mar 29 2010 09:22:52 AM
Investigation of Nonlinear Motion Experienced on a Slender-Wing Research Aircraft c20031012 [7].pdfInvestigation of Nonlinear Motion Experienced on a Slender-Wing Research Aircraft c20031012 [7].pdf 974KB Mar 29 2010 09:22:52 AM
Prediction of the Spectral Content of Combination Tone Noise c20031012 [6].pdfPrediction of the Spectral Content of Combination Tone Noise c20031012 [6].pdf 756KB Mar 29 2010 09:22:52 AM
Reply by Author to W. P. Rodden c20031012 [1].pdfReply by Author to W. P. Rodden c20031012 [1].pdf 104KB Mar 29 2010 09:22:52 AM
Sonic-Boom Wind-Tunnel Testing Techniques at High Mach Numbers c20031012 [4].pdfSonic-Boom Wind-Tunnel Testing Techniques at High Mach Numbers c20031012 [4].pdf 612KB Mar 29 2010 09:22:52 AM