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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1983/1/

Folder.. - Mar 05 2025 11:52:31 PM
Aerodynamic characteristics of a slotted vs smooth-skin supercritical wing model c20030622 [3].pdfAerodynamic characteristics of a slotted vs smooth-skin supercritical wing model c20030622 [3].pdf 420KB Mar 29 2010 10:35:04 AM
A new approach to optimization for aerodynamic applications c20030622 [3].pdfA new approach to optimization for aerodynamic applications c20030622 [3].pdf 365KB Mar 29 2010 10:35:04 AM
A new concept for aircraft dynamic stability testing c20030622 [10].pdfA new concept for aircraft dynamic stability testing c20030622 [10].pdf 1302KB Mar 29 2010 10:35:04 AM
Cast transage 175 titanium alloy for durability critical structural components c20030622 [4].pdfCast transage 175 titanium alloy for durability critical structural components c20030622 [4].pdf 578KB Mar 29 2010 10:35:04 AM
Cross-coupling between longitudinal and lateral aircraft dynamics ina spiral dive c20030622 [6].pdfCross-coupling between longitudinal and lateral aircraft dynamics ina spiral dive c20030622 [6].pdf 666KB Mar 29 2010 10:35:04 AM
Design for global damage tolerance and associated mass penalties c20030622 [6].pdfDesign for global damage tolerance and associated mass penalties c20030622 [6].pdf 839KB Mar 29 2010 10:35:04 AM
Meteorological inputs to flight simulators c20030622 [2].pdfMeteorological inputs to flight simulators c20030622 [2].pdf 351KB Mar 29 2010 10:35:04 AM
Modular asymmetric parachute for wind tunnel testing c20030622 [2].pdfModular asymmetric parachute for wind tunnel testing c20030622 [2].pdf 356KB Mar 29 2010 10:35:04 AM
Novel airborne technique for aircraft noise measurements above the flight path c20030622 [8].pdfNovel airborne technique for aircraft noise measurements above the flight path c20030622 [8].pdf 1614KB Mar 29 2010 10:35:04 AM
Procedure for evaluation of engine isolators for reduced structure-borne noise transmission c20030622 [7].pdfProcedure for evaluation of engine isolators for reduced structure-borne noise transmission c20030622 [7].pdf 1013KB Mar 29 2010 10:35:04 AM
Propeller noise at model- and full-scale c20030622 [8].pdfPropeller noise at model- and full-scale c20030622 [8].pdf 1018KB Mar 29 2010 10:35:04 AM
Reductions in parachute drag due to forebody wake effects c20030622 [8].pdfReductions in parachute drag due to forebody wake effects c20030622 [8].pdf 1128KB Mar 29 2010 10:35:04 AM
Reviewers for the Journal of Aiucruft-l982_ c20030626 [2].pdfReviewers for the Journal of Aiucruft-l982_ c20030626 [2].pdf 247KB Mar 29 2010 10:35:04 AM
Rolls-Royce RB 211-535 Power Plant c20030622 [6].pdfRolls-Royce RB 211-535 Power Plant c20030622 [6].pdf 1005KB Mar 29 2010 10:35:04 AM
Some recent applications of high-lift computational methods at Boeing c20030622 [7].pdfSome recent applications of high-lift computational methods at Boeing c20030622 [7].pdf 947KB Mar 29 2010 10:35:04 AM
TF41 Lamilloy accelerated mission test c20030622 [6].pdfTF41 Lamilloy accelerated mission test c20030622 [6].pdf 1181KB Mar 29 2010 10:35:04 AM
The 1983 Team_ New Policies and Procedures c20030626 [3].pdfThe 1983 Team_ New Policies and Procedures c20030626 [3].pdf 587KB Mar 29 2010 10:35:04 AM
Wind tunnel measurements of blade vane ratio and spacing effects on fan noise c20030622 [8].pdfWind tunnel measurements of blade vane ratio and spacing effects on fan noise c20030622 [8].pdf 966KB Mar 29 2010 10:35:04 AM