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/1983/8/

Folder.. - Mar 05 2025 11:52:31 PM
Durability and damage tolerance control plans for U.S. Air Force aircraft c20030622 [7].pdfDurability and damage tolerance control plans for U.S. Air Force aircraft c20030622 [7].pdf 906KB Mar 29 2010 10:36:30 AM
F A-18 inlet engine compatibility flight test results c20030622 [9].pdfF A-18 inlet engine compatibility flight test results c20030622 [9].pdf 1178KB Mar 29 2010 10:36:30 AM
Finite-element analysis of the T-38 canopy c20030622 [7].pdfFinite-element analysis of the T-38 canopy c20030622 [7].pdf 1046KB Mar 29 2010 10:36:30 AM
Freestream turbulence effects on compressor cascade wake c20030622 [2].pdfFreestream turbulence effects on compressor cascade wake c20030622 [2].pdf 291KB Mar 29 2010 10:36:30 AM
Helicopter IFR approaches into major terminals using RNAV, MLS, and CDTI c20030622 [8].pdfHelicopter IFR approaches into major terminals using RNAV, MLS, and CDTI c20030622 [8].pdf 1284KB Mar 29 2010 10:36:30 AM
Injection slot location for boundary-layer control in shock-induced separation c20030622 [7].pdfInjection slot location for boundary-layer control in shock-induced separation c20030622 [7].pdf 989KB Mar 29 2010 10:36:30 AM
JT9D performance deterioration results from a simulated aerodynamic load test c20030622 [9].pdfJT9D performance deterioration results from a simulated aerodynamic load test c20030622 [9].pdf 1207KB Mar 29 2010 10:36:30 AM
Recent improvements in prediction techniques for supersonic weapon separation c20030622 [7].pdfRecent improvements in prediction techniques for supersonic weapon separation c20030622 [7].pdf 734KB Mar 29 2010 10:36:30 AM
Rigid-body structural mode coupling on a forward swept wing aircraft c20030622 [7].pdfRigid-body structural mode coupling on a forward swept wing aircraft c20030622 [7].pdf 913KB Mar 29 2010 10:36:30 AM
Supersonic three-dimensional oscillatory piecewise continuous kernelfunction method c20030622 [8].pdfSupersonic three-dimensional oscillatory piecewise continuous kernelfunction method c20030622 [8].pdf 966KB Mar 29 2010 10:36:30 AM
The effect of displacement velocity on propeller performance c20030622 [3].pdfThe effect of displacement velocity on propeller performance c20030622 [3].pdf 332KB Mar 29 2010 10:36:30 AM
The role and application of data base management in integrated computer-aided design c20030622 [9].pdfThe role and application of data base management in integrated computer-aided design c20030622 [9].pdf 1117KB Mar 29 2010 10:36:30 AM
Transonic flutter model study of a supercritical wing and winglet c20030622 [6].pdfTransonic flutter model study of a supercritical wing and winglet c20030622 [6].pdf 1045KB Mar 29 2010 10:36:30 AM
Transonic time-response analysis of 3-degree-of-freedom conventionaland supercritical airfoils c20030622 [8].pdfTransonic time-response analysis of 3-degree-of-freedom conventionaland supercritical airfoils c20030622 [8].pdf 1003KB Mar 29 2010 10:36:30 AM