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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1991/11/

Folder.. - Mar 05 2025 11:57:42 PM
Aeroelastic analysis of wings using the Euler equations with a deforming mesh c20030714 [8].pdfAeroelastic analysis of wings using the Euler equations with a deforming mesh c20030714 [8].pdf 2130KB Mar 29 2010 11:01:52 AM
Analysis of flexible-membrane and jet-flapped airfoils using velocity singularities c20030710 [7].pdfAnalysis of flexible-membrane and jet-flapped airfoils using velocity singularities c20030710 [7].pdf 784KB Mar 29 2010 11:01:52 AM
Analysis of unsteady pressures induced on a body by a rotor c20030710 [12].pdfAnalysis of unsteady pressures induced on a body by a rotor c20030710 [12].pdf 1741KB Mar 29 2010 11:01:52 AM
Boundary-layer and wake measurements on a swept, circulation-controlwing c20030710 [7].pdfBoundary-layer and wake measurements on a swept, circulation-controlwing c20030710 [7].pdf 1286KB Mar 29 2010 11:01:52 AM
Computation of three-dimensional turbulent vortical flows on bodies at high incidence c20030710 [11].pdfComputation of three-dimensional turbulent vortical flows on bodies at high incidence c20030710 [11].pdf 1613KB Mar 29 2010 11:01:52 AM
Computation of vectoring nozzle performance c20030711 [6].pdfComputation of vectoring nozzle performance c20030711 [6].pdf 852KB Mar 29 2010 11:01:52 AM
Euler code evaluation of a transatmospheric vehicle at supersonic speeds c20030710 [6].pdfEuler code evaluation of a transatmospheric vehicle at supersonic speeds c20030710 [6].pdf 687KB Mar 29 2010 11:01:52 AM
Experimental investigation on the effect of crescent planform on lift and drag c20030710 [8].pdfExperimental investigation on the effect of crescent planform on lift and drag c20030710 [8].pdf 1249KB Mar 29 2010 11:01:52 AM
Fickle effect of nose microasymmetry on the high-alpha aerodynamics c20030711 [4].pdfFickle effect of nose microasymmetry on the high-alpha aerodynamics c20030711 [4].pdf 474KB Mar 29 2010 11:01:52 AM
Lift development of delta wings undergoing constant acceleration from rest c20030710 [6].pdfLift development of delta wings undergoing constant acceleration from rest c20030710 [6].pdf 923KB Mar 29 2010 11:01:52 AM
Numerical simulation of the actuation system for the ALDF's propulsion control valve c20030710 [6].pdfNumerical simulation of the actuation system for the ALDF's propulsion control valve c20030710 [6].pdf 686KB Mar 29 2010 11:01:52 AM
Poststall airfoil response to a periodic freestream c20030710 [2].pdfPoststall airfoil response to a periodic freestream c20030710 [2].pdf 260KB Mar 29 2010 11:01:52 AM
Probe shapes for streamwise momentum and cross-stream turbulence intensity c20030710 [9].pdfProbe shapes for streamwise momentum and cross-stream turbulence intensity c20030710 [9].pdf 1089KB Mar 29 2010 11:01:52 AM
Probe systems for static pressure and cross-stream turbulence intensity c20030710 [6].pdfProbe systems for static pressure and cross-stream turbulence intensity c20030710 [6].pdf 864KB Mar 29 2010 11:01:52 AM
Supersonic boundary-layer stability analysis on an aircraft wing c20030710 [7].pdfSupersonic boundary-layer stability analysis on an aircraft wing c20030710 [7].pdf 816KB Mar 29 2010 11:01:52 AM
Two-dimensional adaptive-wall tests in the NASA Ames two- by two-foot transonic wind tunnel c20030710 [10].pdfTwo-dimensional adaptive-wall tests in the NASA Ames two- by two-foot transonic wind tunnel c20030710 [10].pdf 1033KB Mar 29 2010 11:01:52 AM
Wall interference assessment correction for transonic airfoil data c20030710 [7].pdfWall interference assessment correction for transonic airfoil data c20030710 [7].pdf 1037KB Mar 29 2010 11:01:52 AM
Wind-tunnel and flight tests of a delta-wing remotely piloted vehicle c20030710 [7].pdfWind-tunnel and flight tests of a delta-wing remotely piloted vehicle c20030710 [7].pdf 982KB Mar 29 2010 11:01:52 AM