Help me if I helped you.
Buy me a beer/coffee!
Keep this site updated!

Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1969/1/

Folder.. - Mar 05 2025 11:44:27 PM
''Power law'' profiles in thermally stratified shear flows. c20031104 [2].pdf''Power law'' profiles in thermally stratified shear flows. c20031104 [2].pdf 251KB Mar 29 2010 09:16:20 AM
A Closed-Form Solution to Oblique Shock-Wave Properties c20031104 [1].pdfA Closed-Form Solution to Oblique Shock-Wave Properties c20031104 [1].pdf 151KB Mar 29 2010 09:16:20 AM
A computer method for dynamic structural analysis using stiffness matrices. c20031104 [6].pdfA computer method for dynamic structural analysis using stiffness matrices. c20031104 [6].pdf 753KB Mar 29 2010 09:16:20 AM
A method of analysis for propellers at extreme angles-of-attack. c20031104 [7].pdfA method of analysis for propellers at extreme angles-of-attack. c20031104 [7].pdf 930KB Mar 29 2010 09:16:20 AM
A new approach to visual simulation. c20031104 [6].pdfA new approach to visual simulation. c20031104 [6].pdf 712KB Mar 29 2010 09:16:20 AM
A new solution for the skin-friction drag on a cylinder. c20031104 [3].pdfA new solution for the skin-friction drag on a cylinder. c20031104 [3].pdf 319KB Mar 29 2010 09:16:20 AM
A strip method for prediction of damping in subsonic wind tunnel andflight flutter tests. c20031104 [9].pdfA strip method for prediction of damping in subsonic wind tunnel andflight flutter tests. c20031104 [9].pdf 1185KB Mar 29 2010 09:16:20 AM
Damping of high-frequency brake vibrations in aircraft landing gear. c20031104 [7].pdfDamping of high-frequency brake vibrations in aircraft landing gear. c20031104 [7].pdf 956KB Mar 29 2010 09:16:20 AM
Development of aircraft vortex wakes in turbulent flow. c20031104 [2].pdfDevelopment of aircraft vortex wakes in turbulent flow. c20031104 [2].pdf 294KB Mar 29 2010 09:16:20 AM
Development of the shim-joint concept for composite structural members. c20031104 [7].pdfDevelopment of the shim-joint concept for composite structural members. c20031104 [7].pdf 901KB Mar 29 2010 09:16:20 AM
Effect of a wing on its tip vortex. c20031104 [5].pdfEffect of a wing on its tip vortex. c20031104 [5].pdf 674KB Mar 29 2010 09:16:20 AM
Experimental research on parachute deployment load control by use ofline ties. c20031104 [2].pdfExperimental research on parachute deployment load control by use ofline ties. c20031104 [2].pdf 591KB Mar 29 2010 09:16:20 AM
Free vibration of simply supported parallelogrammic plates. c20031104 [3].pdfFree vibration of simply supported parallelogrammic plates. c20031104 [3].pdf 420KB Mar 29 2010 09:16:20 AM
High-speed store separation - Correlation between wind-tunnel and flight-test data. c20031106 [4].pdfHigh-speed store separation - Correlation between wind-tunnel and flight-test data. c20031106 [4].pdf 667KB Mar 29 2010 09:16:20 AM
Improvement of ejector-diffuser performance by reduction of backflow. c20031104 [2].pdfImprovement of ejector-diffuser performance by reduction of backflow. c20031104 [2].pdf 304KB Mar 29 2010 09:16:20 AM
Jet-pump actuation of variable-density subsonic wind tunnels. c20031104 [7].pdfJet-pump actuation of variable-density subsonic wind tunnels. c20031104 [7].pdf 868KB Mar 29 2010 09:16:20 AM
Maximum stress of a stiffened circular cylinder under bending. c20031104 [4].pdfMaximum stress of a stiffened circular cylinder under bending. c20031104 [4].pdf 475KB Mar 29 2010 09:16:20 AM
On Being Relevant c20031104 [1].pdfOn Being Relevant c20031104 [1].pdf 179KB Mar 29 2010 09:16:20 AM
Recent flight-test results in deploying a 20- ft-diam ribbon parachute. c20031104 [3].pdfRecent flight-test results in deploying a 20- ft-diam ribbon parachute. c20031104 [3].pdf 456KB Mar 29 2010 09:16:20 AM
Reviewers for Journal of Aircraft, October 1, 1967-September 30, 1968_ c20031104 [1].pdfReviewers for Journal of Aircraft, October 1, 1967-September 30, 1968_ c20031104 [1].pdf 117KB Mar 29 2010 09:16:20 AM
Turbulent Skin-Friction Coefficient and Momentum Thickness in Adverse Pressure Gradient c20031104 [1].pdfTurbulent Skin-Friction Coefficient and Momentum Thickness in Adverse Pressure Gradient c20031104 [1].pdf 134KB Mar 29 2010 09:16:20 AM
Unsteady aerodynamic and stall effects on helicopter rotor blade airfoil sections. c20031106 [6].pdfUnsteady aerodynamic and stall effects on helicopter rotor blade airfoil sections. c20031106 [6].pdf 780KB Mar 29 2010 09:16:20 AM