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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1982/11/
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Mar 05 2025 11:51:45 PM
Advanced facility for processing aircraft dynamic test data c20040813 [9].pdf
1309KB
Mar 29 2010 10:34:18 AM
Air bag impact attenuation system for the AQM-34V remote piloted vehicle c20040813 [6].pdf
1284KB
Mar 29 2010 10:34:18 AM
Analysis and flight data for a drone aircraft with active flutter suppression c20040813 [7].pdf
807KB
Mar 29 2010 10:34:18 AM
Application of pulse code modulation technology to aircraft dynamicsdata acquisition c20040813 [6].pdf
776KB
Mar 29 2010 10:34:18 AM
Combat survivability with advanced aircraft propulsion development c20040813 [6].pdf
952KB
Mar 29 2010 10:34:18 AM
Comparison of computational and experimental jet effects c20040813 [6].pdf
643KB
Mar 29 2010 10:34:18 AM
Critique of the Gravity Vector Alignment Method for Motion Simulation c20040813 [4].pdf
421KB
Mar 29 2010 10:34:18 AM
Departure susceptibility and uncoordinated roll-reversal boundaries for fighter configurations c20040813 [7].pdf
746KB
Mar 29 2010 10:34:18 AM
Detection of clear air turbulence using a diagnostic Richardson number tendency formulation c20040813 [5].pdf
611KB
Mar 29 2010 10:34:18 AM
Development of New Lifting-Parachute Designs with Increased Trim Angle c20040813 [7].pdf
987KB
Mar 29 2010 10:34:18 AM
Estimation of aircraft fuel consumption c20040813 [7].pdf
842KB
Mar 29 2010 10:34:18 AM
Flow visualization reveals causes of Shuttle nonlinear aerodynamics c20040813 [6].pdf
2053KB
Mar 29 2010 10:34:18 AM
Ice detector evaluation for aircraft hazard warning and undercooled water content measurements c20040813 [4].pdf
540KB
Mar 29 2010 10:34:18 AM
Improved g-cueing system c20040813 [6].pdf
1102KB
Mar 29 2010 10:34:18 AM
In-flight structural dynamic characteristics of the XV-15 tilt-rotorresearch aircraft c20040813 [7].pdf
810KB
Mar 29 2010 10:34:18 AM
Load distribution on deformed wings in supersonic flow c20040813 [7].pdf
768KB
Mar 29 2010 10:34:18 AM
Prediction of transonic flutter for a supercritical wing by modifiedstrip analysis c20040813 [6].pdf
635KB
Mar 29 2010 10:34:18 AM
Rotor wake characteristics relevant to rotor-stator interaction noise generation c20040813 [9].pdf
1293KB
Mar 29 2010 10:34:18 AM
Swept composite wing aeroelastic divergence experiments c20040813 [6].pdf
787KB
Mar 29 2010 10:34:18 AM
Tests of a thermal acoustic shield with a supersonic jet c20040813 [7].pdf
761KB
Mar 29 2010 10:34:18 AM