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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1983/9/

Folder.. - Mar 05 2025 11:52:31 PM
Aerodynamic aspects of aircraft dynamics at high angles of attack c20030622 [16].pdfAerodynamic aspects of aircraft dynamics at high angles of attack c20030622 [16].pdf 2085KB Mar 29 2010 10:36:46 AM
Aeroservoelasticity in the time domain c20030622 [9].pdfAeroservoelasticity in the time domain c20030622 [9].pdf 1090KB Mar 29 2010 10:36:46 AM
Aircraft trajectories for reduced noise impact c20030622 [7].pdfAircraft trajectories for reduced noise impact c20030622 [7].pdf 857KB Mar 29 2010 10:36:46 AM
Analysis of aircraft dynamic behavior in a crash environment c20030622 [8].pdfAnalysis of aircraft dynamic behavior in a crash environment c20030622 [8].pdf 1394KB Mar 29 2010 10:36:46 AM
Apparent-mass coefficients for isosceles triangles and cross sections formed by two circles c20030622 [7].pdfApparent-mass coefficients for isosceles triangles and cross sections formed by two circles c20030622 [7].pdf 721KB Mar 29 2010 10:36:46 AM
Bonded aluminum honeycomb - Aircraft flight surface primary structure application c20030622 [5].pdfBonded aluminum honeycomb - Aircraft flight surface primary structure application c20030622 [5].pdf 1151KB Mar 29 2010 10:36:46 AM
Design Optimization Codes for Structures - DOCS computer program c20030622 [8].pdfDesign Optimization Codes for Structures - DOCS computer program c20030622 [8].pdf 1060KB Mar 29 2010 10:36:46 AM
Interior noise considerations for advanced high-speed turboprop aircraft c20030622 [7].pdfInterior noise considerations for advanced high-speed turboprop aircraft c20030622 [7].pdf 1306KB Mar 29 2010 10:36:46 AM
Moisture and temperature effects on the instability of cylindrical composite panels c20030622 [7].pdfMoisture and temperature effects on the instability of cylindrical composite panels c20030622 [7].pdf 949KB Mar 29 2010 10:36:46 AM
Optimum configuration for a 10-passenger business turbofan jet airplane c20030622 [7].pdfOptimum configuration for a 10-passenger business turbofan jet airplane c20030622 [7].pdf 924KB Mar 29 2010 10:36:46 AM
Preliminary supersonic analysis methods including high angle of attack c20030622 [7].pdfPreliminary supersonic analysis methods including high angle of attack c20030622 [7].pdf 869KB Mar 29 2010 10:36:46 AM
Vortex flow over delta and double-delta wings c20030622 [8].pdfVortex flow over delta and double-delta wings c20030622 [8].pdf 1262KB Mar 29 2010 10:36:46 AM