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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1984/6/

Folder.. - Mar 05 2025 11:53:19 PM
Aerodynamics of pointed forebodies at high angles of attack c20030718 [5].pdfAerodynamics of pointed forebodies at high angles of attack c20030718 [5].pdf 570KB Mar 29 2010 10:39:16 AM
An experimental investigation of VTOL flying qualities requirements in shipboard landings c20030718 [9].pdfAn experimental investigation of VTOL flying qualities requirements in shipboard landings c20030718 [9].pdf 1209KB Mar 29 2010 10:39:16 AM
Application of computational aerodynamics to airplane design c20030718 [16].pdfApplication of computational aerodynamics to airplane design c20030718 [16].pdf 2183KB Mar 29 2010 10:39:16 AM
Calculation of potential flow past simple bodies using axial sourcesand a least-squares method c20030718 [2].pdfCalculation of potential flow past simple bodies using axial sourcesand a least-squares method c20030718 [2].pdf 244KB Mar 29 2010 10:39:16 AM
Computation of transonic flow around airfoils with trailing edge andshock boundary layer interactions c20030718 [9].pdfComputation of transonic flow around airfoils with trailing edge andshock boundary layer interactions c20030718 [9].pdf 813KB Mar 29 2010 10:39:16 AM
Design and experimental verification of the USB flap panel structurefor NAL-STOL research aircraft c20030718 [2].pdfDesign and experimental verification of the USB flap panel structurefor NAL-STOL research aircraft c20030718 [2].pdf 207KB Mar 29 2010 10:39:16 AM
Divergence boundary prediction from random responses - NAL's method c20030718 [2].pdfDivergence boundary prediction from random responses - NAL's method c20030718 [2].pdf 286KB Mar 29 2010 10:39:16 AM
Efficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices c20030718 [3].pdfEfficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices c20030718 [3].pdf 379KB Mar 29 2010 10:39:16 AM
Engineering analysis of drooped leading-edge wings near stall c20030718 [3].pdfEngineering analysis of drooped leading-edge wings near stall c20030718 [3].pdf 403KB Mar 29 2010 10:39:16 AM
Errata_ _A Computer System for Aircraft Flyover Acoustic Data Acquisition and Analysis_ c20030718 [1].pdfErrata_ _A Computer System for Aircraft Flyover Acoustic Data Acquisition and Analysis_ c20030718 [1].pdf 94KB Mar 29 2010 10:39:16 AM
Measurements of ground effect for delta wings c20030718 [3].pdfMeasurements of ground effect for delta wings c20030718 [3].pdf 365KB Mar 29 2010 10:39:16 AM
On the convergence of unsteady generalized aerodynamic forces c20030718 [8].pdfOn the convergence of unsteady generalized aerodynamic forces c20030718 [8].pdf 848KB Mar 29 2010 10:39:16 AM
Profile drag from laser-Doppler velocimeter measurement c20030718 [3].pdfProfile drag from laser-Doppler velocimeter measurement c20030718 [3].pdf 350KB Mar 29 2010 10:39:16 AM
Specification, design, and test of aircraft engine isolators for reduced interior noise c20030718 [8].pdfSpecification, design, and test of aircraft engine isolators for reduced interior noise c20030718 [8].pdf 1147KB Mar 29 2010 10:39:16 AM
Thrust reverser exhaust plume reingestion model tests c20030718 [7].pdfThrust reverser exhaust plume reingestion model tests c20030718 [7].pdf 753KB Mar 29 2010 10:39:16 AM
Thrust vector control of a V STOL airship c20030718 [6].pdfThrust vector control of a V STOL airship c20030718 [6].pdf 812KB Mar 29 2010 10:39:16 AM
Two-dimensional wind-tunnel interference from measurements on two contours c20030718 [6].pdfTwo-dimensional wind-tunnel interference from measurements on two contours c20030718 [6].pdf 635KB Mar 29 2010 10:39:16 AM
Unsteady pressures and forces during transonic buffeting of a supercritical airfoil c20030718 [3].pdfUnsteady pressures and forces during transonic buffeting of a supercritical airfoil c20030718 [3].pdf 336KB Mar 29 2010 10:39:16 AM
Worldwide aviation outlook c20030718 [4].pdfWorldwide aviation outlook c20030718 [4].pdf 466KB Mar 29 2010 10:39:16 AM