Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1975/2/

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Acknowledgments with Gratitude c20040109 [1].pdf 114KB Mar 29 2010 10:04:18 AM

Aircraft vortex detection system using dual laser beams c20040109 [2].pdf 315KB Mar 29 2010 10:04:18 AM

Approximate solution of minimum induced drag of wings with given structural weight c20040109 [3].pdf 318KB Mar 29 2010 10:04:18 AM

Comment on 'Exact method of designing airfoils with given velocity distribution in incompressible flow' c20040109 [1].pdf 170KB Mar 29 2010 10:04:18 AM

Dynamic Effects of Shock-Induced Flow Separation c20040109 [7].pdf 830KB Mar 29 2010 10:04:18 AM

Effect of heating on leading edge vortices in subsonic flow c20040109 [3].pdf 400KB Mar 29 2010 10:04:18 AM

Effects of Compressive Overloads on Fatigue Crack Growth c20040109 [5].pdf 624KB Mar 29 2010 10:04:18 AM

Evaluation of Damage Tolerance in Aircraft Structures c20040109 [7].pdf 1008KB Mar 29 2010 10:04:18 AM

Generalized integrated square error criterion for optimal and suboptimal control design c20040109 [5].pdf 501KB Mar 29 2010 10:04:18 AM

Iterative techniques for the solution of large linear systems in computational aerodynamics c20040109 [3].pdf 361KB Mar 29 2010 10:04:18 AM

Operating and Ambient Condition Influences on Aircraft Gas Turbine NOX Emissions c20040109 [6].pdf 802KB Mar 29 2010 10:04:18 AM

Prediction of airfoil tone frequencies c20040109 [3].pdf 352KB Mar 29 2010 10:04:18 AM

Pressure field of a vortex wake in ground effect c20040109 [2].pdf 236KB Mar 29 2010 10:04:18 AM

Reply by Author to R. H. Liebeck c20040109 [2].pdf 258KB Mar 29 2010 10:04:18 AM

Separated flow over a body of revolution c20040109 [8].pdf 964KB Mar 29 2010 10:04:18 AM

Transonic Study of Active Flutter Suppression Based on an Energy Concept c20040109 [6].pdf 915KB Mar 29 2010 10:04:18 AM

Verification of the Heat-Field Concept for Sonic-Boom Alleviation c20040109 [6].pdf 708KB Mar 29 2010 10:04:18 AM