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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1973/5/

Folder.. - Mar 05 2025 11:46:26 PM
Advanced supersonic inlet technology. c20031012 [5].pdfAdvanced supersonic inlet technology. c20031012 [5].pdf 752KB Mar 29 2010 09:24:20 AM
Advanced Technology Applications to Present and Future Transport Aircraft c20031012 [8].pdfAdvanced Technology Applications to Present and Future Transport Aircraft c20031012 [8].pdf 1414KB Mar 29 2010 09:24:20 AM
Aerodynamic Loading on High-Speed Ground Vehicles c20031012 [2].pdfAerodynamic Loading on High-Speed Ground Vehicles c20031012 [2].pdf 271KB Mar 29 2010 09:24:20 AM
Analysis of the Interaction of Jets and Airfoils in Two Dimensions c20031012 [7].pdfAnalysis of the Interaction of Jets and Airfoils in Two Dimensions c20031012 [7].pdf 916KB Mar 29 2010 09:24:20 AM
A Perturbation Solution of Helicopter Rotor Flapping Stability c20031012 [2].pdfA Perturbation Solution of Helicopter Rotor Flapping Stability c20031012 [2].pdf 303KB Mar 29 2010 09:24:20 AM
A simple estimate of the effect of ejector length on thrust augmentation. c20031012 [2].pdfA simple estimate of the effect of ejector length on thrust augmentation. c20031012 [2].pdf 267KB Mar 29 2010 09:24:20 AM
Complex Coordinates in Near Hovering Rotor Dynamics c20031012 [8].pdfComplex Coordinates in Near Hovering Rotor Dynamics c20031012 [8].pdf 1038KB Mar 29 2010 09:24:20 AM
Errata-Drift of Buoyant Wing-Tip Vortices c20031012 [1].pdfErrata-Drift of Buoyant Wing-Tip Vortices c20031012 [1].pdf 87KB Mar 29 2010 09:24:20 AM
Nonplanar wings in nonplanar ground effect. c20031012 [5].pdfNonplanar wings in nonplanar ground effect. c20031012 [5].pdf 718KB Mar 29 2010 09:24:20 AM
Normal mode solution to the equations of motion of a flexible airplane. c20031012 [3].pdfNormal mode solution to the equations of motion of a flexible airplane. c20031012 [3].pdf 365KB Mar 29 2010 09:24:20 AM
Prediction of Inlet Duct Overpressures Resulting from Engine Surge c20031012 [5].pdfPrediction of Inlet Duct Overpressures Resulting from Engine Surge c20031012 [5].pdf 695KB Mar 29 2010 09:24:20 AM
Quasi-Linearizatioh Technique for Estimating Aircraft States from Flight Data c20031012 [5].pdfQuasi-Linearizatioh Technique for Estimating Aircraft States from Flight Data c20031012 [5].pdf 626KB Mar 29 2010 09:24:20 AM
Remarks on vortex-lattice methods. c20031012 [4].pdfRemarks on vortex-lattice methods. c20031012 [4].pdf 529KB Mar 29 2010 09:24:20 AM
Target-Type Thrust Reverser Noise c20031012 [6].pdfTarget-Type Thrust Reverser Noise c20031012 [6].pdf 717KB Mar 29 2010 09:24:20 AM
Vortex Noise of Isolated Airfoils c20031012 [7].pdfVortex Noise of Isolated Airfoils c20031012 [7].pdf 1049KB Mar 29 2010 09:24:20 AM