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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1969/6/

Folder.. - Mar 05 2025 11:44:27 PM
A comparison of C-141A flight test measured and theoretical vertical-gust responses c20031104 [5].pdfA comparison of C-141A flight test measured and theoretical vertical-gust responses c20031104 [5].pdf 590KB Mar 29 2010 09:17:16 AM
A method for predicting longitudinal stability derivatives of rigid and elastic airplanes c20031104 [7].pdfA method for predicting longitudinal stability derivatives of rigid and elastic airplanes c20031104 [7].pdf 766KB Mar 29 2010 09:17:16 AM
Analysis of damaged structure c20031104 [3].pdfAnalysis of damaged structure c20031104 [3].pdf 408KB Mar 29 2010 09:17:16 AM
Change in pitching-moment coefficient due to ground effect c20031104 [2].pdfChange in pitching-moment coefficient due to ground effect c20031104 [2].pdf 310KB Mar 29 2010 09:17:16 AM
Determination of the wake behind a bluff body of revolution at high Reynolds numbers c20031104 [3].pdfDetermination of the wake behind a bluff body of revolution at high Reynolds numbers c20031104 [3].pdf 438KB Mar 29 2010 09:17:16 AM
Dynamics of a multiple-skirt air cushion vehicle c20031106 [2].pdfDynamics of a multiple-skirt air cushion vehicle c20031106 [2].pdf 402KB Mar 29 2010 09:17:16 AM
Effects of vortex separation on the lift distribution on bodies of elliptic cross section c20031104 [7].pdfEffects of vortex separation on the lift distribution on bodies of elliptic cross section c20031104 [7].pdf 920KB Mar 29 2010 09:17:16 AM
Energy-state approximation in performance optimization of supersonicaircraft c20031104 [8].pdfEnergy-state approximation in performance optimization of supersonicaircraft c20031104 [8].pdf 900KB Mar 29 2010 09:17:16 AM
Estimation of aerodynamic center and span load distributions of swept wings c20031104 [3].pdfEstimation of aerodynamic center and span load distributions of swept wings c20031104 [3].pdf 392KB Mar 29 2010 09:17:16 AM
Fail-safe criteria and analysis of VTOL dynamic component structures c20031104 [3].pdfFail-safe criteria and analysis of VTOL dynamic component structures c20031104 [3].pdf 308KB Mar 29 2010 09:17:16 AM
Flapping response of lifting rotor blades to atmospheric turbulence c20031104 [8].pdfFlapping response of lifting rotor blades to atmospheric turbulence c20031104 [8].pdf 1000KB Mar 29 2010 09:17:16 AM
Flying qualities - An integral part of a stability augmentation system c20031104 [6].pdfFlying qualities - An integral part of a stability augmentation system c20031104 [6].pdf 799KB Mar 29 2010 09:17:16 AM
Gross thrust coefficient - Turbofan engines c20031106 [2].pdfGross thrust coefficient - Turbofan engines c20031106 [2].pdf 419KB Mar 29 2010 09:17:16 AM
Lifting surface theory for V STOL aircraft in transition and cruise. I c20031104 [8].pdfLifting surface theory for V STOL aircraft in transition and cruise. I c20031104 [8].pdf 897KB Mar 29 2010 09:17:16 AM
On the singularity method of subsonic lifting- surface theory c20031104 [10].pdfOn the singularity method of subsonic lifting- surface theory c20031104 [10].pdf 1141KB Mar 29 2010 09:17:16 AM
Peripheral jets - Effect of exit geometry c20031104 [6].pdfPeripheral jets - Effect of exit geometry c20031104 [6].pdf 1072KB Mar 29 2010 09:17:16 AM
Pilot's response to stability augmentation system failures and implications for design c20031104 [6].pdfPilot's response to stability augmentation system failures and implications for design c20031104 [6].pdf 743KB Mar 29 2010 09:17:16 AM
Propagation of error in the calculation of airplane thrust and drag c20031104 [6].pdfPropagation of error in the calculation of airplane thrust and drag c20031104 [6].pdf 603KB Mar 29 2010 09:17:16 AM
Simplified design equations for buckling of axially compressed sandwich cylinders with orthotropic facings and core c20031104 [5].pdfSimplified design equations for buckling of axially compressed sandwich cylinders with orthotropic facings and core c20031104 [5].pdf 631KB Mar 29 2010 09:17:16 AM