Improved Aerodynamic Analysis for Hybrid Wing Body Conceptual Design Optimization [PDF]
This paper provides an overview of ongoing efforts to develop, evaluate, and validate different tools for improved aerodynamic modeling and systems analysis of Hybrid Wing Body (HWB) aircraft configurations. Results are being presented for the evaluation
Gern, Frank H.
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Applications of vortex lattice theory to preliminary aerodynamic design [PDF]
Some applications of the vortex-lattice theory to the preliminary aerodynamic design and analysis of subsonic aircraft were presented. These methods include the Rockwell-Tulinius vortex-lattice theory for estimating aerodynamic characteristics, a Trefftz
Paulson, J. W., Jr.
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Tip aerodynamics from wind tunnel test of semi-span wing [PDF]
Presented are the results of a low-speed wind tunnel test on a 5.33-aspect-ratio, semi-span wing with 30- and 35 deg swept tapered tips. The test results include aerodynamic data for the tip itself and for the entire wing including the tip.
Stroub, Robert H., Vanaken, Johannes M.
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Effects of Angle of Attack, Aspect Ratio, and Leading-Edge Curvature on Supersonic Fin Performance
The aerodynamic optimization of fin-stabilized rockets operating under supersonic conditions remains a critical challenge in aerospace enginnering. Current studies often fail to capture the combined effects of multiple geometric parameters on aerodynamic
M. Hasbi Ash Shiddieqy, Andoko Andoko
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An aerodynamic study of scramjet fuel injectors [PDF]
The aerodynamic drag and fuel distribution patterns of injectors designed for a supersonic combustion ramjet were measured at Mach numbers of 2, 2.5, and 3. The most significant parameter effecting the drag was found to be the injector thickness ratio. A
Povinelli, L. A.
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AERODYNAMIC DRAG AND STABILITY CHARACTERISTICS OF TOWED INFLATABLE DECELERATORS AT SUPERSONIC SPEEDS [PDF]
Aerodynamic drag and stability of towed inflatable decelerators at supersonic ...
Mc Shera, J. T., Jr.
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Validity and Reliability of an On-Bike Sensor System for the Determination of Aerodynamic Drag in Cycling. [PDF]
Hopker JG +3 more
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Numerical investigation of co-flow jet integration to enhance the aerodynamic efficiency of airfoils used in wind turbine applications. [PDF]
Farghaly MB +3 more
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Parametric Optimization of VLM Panel Discretization Using Bio-Inspired Crayfish and Aquila Algorithms Coupled with Hybrid RSM-Based Ensemble Machine Learning Surrogate Models: A Case Study. [PDF]
Eraslan Y, Şengün E.
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Investigation of Drag Reduction Technologies for Light-Duty Vehicles Using Surface, Wake and Underbody Pressure Measurements to Complement Aerodynamic Drag Measurements. [PDF]
de Souza F +4 more
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