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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1986/11/

Folder.. - Mar 05 2025 11:54:37 PM
ADAM - An aeroservoelastic analysis method for analog or digital systems c20030731 [7].pdfADAM - An aeroservoelastic analysis method for analog or digital systems c20030731 [7].pdf 996KB Mar 29 2010 10:49:16 AM
Density stratification effects on wake vortex decay c20030731 [5].pdfDensity stratification effects on wake vortex decay c20030731 [5].pdf 820KB Mar 29 2010 10:49:16 AM
Equivalent plate analysis of aircraft wing box structures with general planform geometry c20030731 [6].pdfEquivalent plate analysis of aircraft wing box structures with general planform geometry c20030731 [6].pdf 817KB Mar 29 2010 10:49:16 AM
Fighter evasive maneuvers against proportional navigation missile c20030731 [6].pdfFighter evasive maneuvers against proportional navigation missile c20030731 [6].pdf 591KB Mar 29 2010 10:49:16 AM
Measurement and prediction of model-rotor flowfields c20030731 [9].pdfMeasurement and prediction of model-rotor flowfields c20030731 [9].pdf 798KB Mar 29 2010 10:49:16 AM
Nonlinear aerodynamics of a two-dimensional membrane airfoil with separation c20030731 [6].pdfNonlinear aerodynamics of a two-dimensional membrane airfoil with separation c20030731 [6].pdf 728KB Mar 29 2010 10:49:16 AM
Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowing c20030731 [7].pdfPerformance augmentation of a 60-degree delta aircraft configurationby spanwise blowing c20030731 [7].pdf 951KB Mar 29 2010 10:49:16 AM
Self-induced roll oscillations measured on a delta wing canard configuration c20030731 [6].pdfSelf-induced roll oscillations measured on a delta wing canard configuration c20030731 [6].pdf 606KB Mar 29 2010 10:49:16 AM
Theoretical prediction of roll moment on wing-controlled missile c20030731 [6].pdfTheoretical prediction of roll moment on wing-controlled missile c20030731 [6].pdf 685KB Mar 29 2010 10:49:16 AM
Transonic separated solutions for an augmentor wing c20030731 [6].pdfTransonic separated solutions for an augmentor wing c20030731 [6].pdf 799KB Mar 29 2010 10:49:16 AM