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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1971/7/

Folder.. - Mar 05 2025 11:45:25 PM
A comparative study of three axisymmetric inlets for a hypersonic cruise mission c20031007 [7].pdfA comparative study of three axisymmetric inlets for a hypersonic cruise mission c20031007 [7].pdf 1083KB Mar 29 2010 09:19:58 AM
Advantage of testing aircraft rotor models with sharply deflected wakes in water c20031007 [2].pdfAdvantage of testing aircraft rotor models with sharply deflected wakes in water c20031007 [2].pdf 337KB Mar 29 2010 09:19:58 AM
Airplane Economic Design Evaluation (AEDE) Computerized Model and Its Application c20031007 [4].pdfAirplane Economic Design Evaluation (AEDE) Computerized Model and Its Application c20031007 [4].pdf 583KB Mar 29 2010 09:19:58 AM
Application of Random Data Techniques to Aircraft Inlet Diagnostics c20031007 [9].pdfApplication of Random Data Techniques to Aircraft Inlet Diagnostics c20031007 [9].pdf 1248KB Mar 29 2010 09:19:58 AM
Computer Aided Stabilator Design Including Aeroelastic Constraints c20031007 [8].pdfComputer Aided Stabilator Design Including Aeroelastic Constraints c20031007 [8].pdf 1163KB Mar 29 2010 09:19:58 AM
Correlation of Turbofan Engine Thrust Performance with Comnound Nozzle Flow Theorv c20031007 [7].pdfCorrelation of Turbofan Engine Thrust Performance with Comnound Nozzle Flow Theorv c20031007 [7].pdf 987KB Mar 29 2010 09:19:58 AM
DC-10 Test Program Effectiveness c20031007 [9].pdfDC-10 Test Program Effectiveness c20031007 [9].pdf 1632KB Mar 29 2010 09:19:58 AM
Dynamic Stall Simulation Problems c20031007 [5].pdfDynamic Stall Simulation Problems c20031007 [5].pdf 646KB Mar 29 2010 09:19:58 AM
Effects of Leading-Edge Vortex Flow on the Roll Damping of Slender Wings c20031007 [5].pdfEffects of Leading-Edge Vortex Flow on the Roll Damping of Slender Wings c20031007 [5].pdf 763KB Mar 29 2010 09:19:58 AM
General instability of eccentrically stiffened cylindrical panels c20031007 [7].pdfGeneral instability of eccentrically stiffened cylindrical panels c20031007 [7].pdf 793KB Mar 29 2010 09:19:58 AM
Jet Flap Diffuser_ A New Thrust Amplifying Device c20031007 [5].pdfJet Flap Diffuser_ A New Thrust Amplifying Device c20031007 [5].pdf 638KB Mar 29 2010 09:19:58 AM
Minimum Weight Design of Stiffened Fiber Composite Cylinders c20031007 [8].pdfMinimum Weight Design of Stiffened Fiber Composite Cylinders c20031007 [8].pdf 1119KB Mar 29 2010 09:19:58 AM
Powered -Engine Simulator Procedures and Experience for the DC-10 Wing Engine c20031007 [7].pdfPowered -Engine Simulator Procedures and Experience for the DC-10 Wing Engine c20031007 [7].pdf 1299KB Mar 29 2010 09:19:58 AM
Recent Experience with Techniques for Prediction of Spin Characteristics of Fighter Aircraft c20031007 [6].pdfRecent Experience with Techniques for Prediction of Spin Characteristics of Fighter Aircraft c20031007 [6].pdf 946KB Mar 29 2010 09:19:58 AM
Reduction of Tractor-Trailer Cross- Wind Response c20031007 [3].pdfReduction of Tractor-Trailer Cross- Wind Response c20031007 [3].pdf 459KB Mar 29 2010 09:19:58 AM
Seeking a New Precision Approach and Landing System-A Test of Maturity c20031009 [5].pdfSeeking a New Precision Approach and Landing System-A Test of Maturity c20031009 [5].pdf 958KB Mar 29 2010 09:19:58 AM
Studies of Engine-Airframe Integration on Hypersonic Aircraft c20031007 [7].pdfStudies of Engine-Airframe Integration on Hypersonic Aircraft c20031007 [7].pdf 983KB Mar 29 2010 09:19:58 AM