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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1996/3/
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Mar 06 2025 12:02:10 AM
Airfoil design utilizing parallel processors c20030728 [3].pdf
432KB
Mar 27 2010 11:45:58 PM
Analytical expression of induced drag for a finite elliptic wing c20030728 [3].pdf
369KB
Mar 27 2010 11:45:58 PM
Approximate formula for the frequencies of a rotating Timoshenko beam c20030728 [3].pdf
393KB
Mar 27 2010 11:45:58 PM
Assessment of noise control measures for a model advanced ducted propulsor c20030728 [6].pdf
1170KB
Mar 27 2010 11:45:58 PM
Comparison of F A-18A inlet flow analyses with flight data. I c20030728 [6].pdf
875KB
Mar 27 2010 11:45:58 PM
Comparison of the F A-18A inlet flow analysis with flight data. II c20030728 [7].pdf
1140KB
Mar 27 2010 11:45:58 PM
Computational environment for exhaust nozzle design c20030728 [7].pdf
1061KB
Mar 27 2010 11:45:58 PM
Damage tolerance and failure analysis of a composite geodesically stiffened compression panel c20030728 [7].pdf
1117KB
Mar 27 2010 11:45:58 PM
Determination of aircraft stall margins during takeoff c20030728 [4].pdf
527KB
Mar 27 2010 11:45:58 PM
Difficulties in predicting vortex breakdown effects on a rolling delta wing c20030728 [8].pdf
825KB
Mar 27 2010 11:45:58 PM
Dynamic response of an axially loaded bending-torsion coupled beam c20030728 [7].pdf
680KB
Mar 27 2010 11:45:58 PM
Errata_ Helicopter Flight Data Feature Extraction for Component Load Monitoring c20030728 [1].pdf
30KB
Mar 27 2010 11:45:58 PM
Evaluation of transition in flight tests using nonlinear parabolized stability equation analysis c20030728 [7].pdf
965KB
Mar 27 2010 11:45:58 PM
F-15 forebody vortex flow control using jet nozzle blowing c20030728 [8].pdf
891KB
Mar 27 2010 11:45:58 PM
Flight test certification of multipurpose head-up display for general aviation aircraft c20030728 [7].pdf
1105KB
Mar 27 2010 11:45:58 PM
Full-scale wind-tunnel studies of F A-18 tail buffet c20030728 [7].pdf
931KB
Mar 27 2010 11:45:58 PM
High-lift design optimization using Navier-Stokes equations c20030728 [6].pdf
823KB
Mar 27 2010 11:45:58 PM
Identification of lateral-directional behavior in stall from flight data c20030728 [4].pdf
614KB
Mar 27 2010 11:45:58 PM
Launch vehicle acoustics. I - Overall levels and spectral characteristics c20030728 [7].pdf
1073KB
Mar 27 2010 11:45:58 PM
Launch vehicle acoustics. II - Statistics of the time domain data c20030728 [6].pdf
769KB
Mar 27 2010 11:45:58 PM
Mathematical simulation of near-vertical flight of fixed-wing aircraft c20030728 [4].pdf
548KB
Mar 27 2010 11:45:58 PM
Multiple design point optimization of high-speed proprotors c20030728 [3].pdf
479KB
Mar 27 2010 11:45:58 PM
Navier-Stokes computations on flexible advanced transport wings in transonic regime c20030728 [6].pdf
808KB
Mar 27 2010 11:45:58 PM
Numerical approach to blade-vortex interaction in two-dimensional viscous flow c20030728 [3].pdf
427KB
Mar 27 2010 11:45:58 PM
Optimal rectangular end plates c20030728 [3].pdf
439KB
Mar 27 2010 11:45:58 PM
Parallel computational fluid dynamics design on network-based computer c20030728 [6].pdf
742KB
Mar 27 2010 11:45:58 PM
Pitch rate effects on delta wing vortex breakdown c20030728 [4].pdf
456KB
Mar 27 2010 11:45:58 PM
Reduction of vertical tail buffet response using active control c20030728 [6].pdf
1026KB
Mar 27 2010 11:45:58 PM
Sailplane carry-through structures made with composite materials c20030728 [5].pdf
575KB
Mar 27 2010 11:45:58 PM
Simultaneous optimization of sailplane design and its flight trajectory c20030728 [5].pdf
612KB
Mar 27 2010 11:45:58 PM
Structural weight estimation for multidisciplinary optimization of a high-speed civil transport c20030728 [9].pdf
1071KB
Mar 27 2010 11:45:58 PM
Time-averaged active controller for turbofan engine fan noise reduction c20030728 [8].pdf
1123KB
Mar 27 2010 11:45:58 PM
Vortex model to define safe aircraft separation distances c20030728 [7].pdf
823KB
Mar 27 2010 11:45:58 PM
Wake-vortex separation distances when flight-path corridors are constrained c20030728 [8].pdf
1182KB
Mar 27 2010 11:45:58 PM
Water vapor transmission through hull material and buoyancy of aerostats c20030728 [4].pdf
403KB
Mar 27 2010 11:45:58 PM
X-31A system identification using single-surface excitation at high angles of attack c20030728 [6].pdf
678KB
Mar 27 2010 11:45:58 PM