Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1975/10/

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Analytical Prediction of Store Separation Characteristics from Subsonic Aircraft c20040126 [7].pdf 748KB Mar 29 2010 10:05:48 AM

Conceptual Design of a Lift Fan Plus Lift Cruise Fighter Aircraft c20040126 [6].pdf 806KB Mar 29 2010 10:05:48 AM

Dual-phase damping in a landing gear at touch-down c20040126 [3].pdf 319KB Mar 29 2010 10:05:48 AM

Dynamic stability of a translating vehicle with a simple sling load c20040126 [5].pdf 602KB Mar 29 2010 10:05:48 AM

Effect of Wind Shear and Ground Plane on Aircraft Wake Vortices c20040126 [4].pdf 426KB Mar 29 2010 10:05:48 AM

Engine Flow Diverter System for the XFV-12A Prototype Aircraft c20040126 [7].pdf 902KB Mar 29 2010 10:05:48 AM

Errata_ Some Aspects of Fan Noise Suppression Using High Mach Number Inlets c20040126 [1].pdf 87KB Mar 29 2010 10:05:48 AM

General Aviation Application of Separate Surface Stability Augmentation c20040126 [4].pdf 591KB Mar 29 2010 10:05:48 AM

Improvements in Airplane Stopping Performance on Adverse Runways c20040126 [4].pdf 625KB Mar 29 2010 10:05:48 AM

Influence of Rainfall Intensity on Erosion of Materials at Supersonic Velocities c20040126 [2].pdf 287KB Mar 29 2010 10:05:48 AM

Large Fracture Toughness Boron-Epoxy Composites c20040126 [3].pdf 348KB Mar 29 2010 10:05:48 AM

Note on stability in decelerating flight c20040126 [2].pdf 222KB Mar 29 2010 10:05:48 AM

Performance of small skin friction balances at supersonic speeds c20040126 [7].pdf 955KB Mar 29 2010 10:05:48 AM

Prediction of Compressor Stall for Distorted and Undistorted Inlet Flow c20040126 [6].pdf 706KB Mar 29 2010 10:05:48 AM

Simulation and Analysis of a Demand Responsive, Automated Transit System c20040126 [4].pdf 589KB Mar 29 2010 10:05:48 AM

Simulation Study of an Aircraft's Environmental Control System Dynamic Response c20040126 [2].pdf 294KB Mar 29 2010 10:05:48 AM

Solution of the Lane-Friedman integral equation c20040126 [9].pdf 845KB Mar 29 2010 10:05:48 AM

Static Aerodynamics of Missile Configurations for Mach O to 3 c20040126 [10].pdf 1135KB Mar 29 2010 10:05:48 AM

Status and Benefits of Instrumented Two-Segment Approaches; August, 1974 c20040126 [6].pdf 954KB Mar 29 2010 10:05:48 AM

Theoretical Store Separation Analyses of a Prototype Store c20040126 [5].pdf 872KB Mar 29 2010 10:05:48 AM

Wing-Slipstream Interaction with Mach Number Nonuniformity c20040126 [2].pdf 236KB Mar 29 2010 10:05:48 AM