Results 101 to 110 of about 84,328 (206)

Improved Aerodynamic Analysis for Hybrid Wing Body Conceptual Design Optimization [PDF]

open access: yes, 2012
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.
core   +1 more source

Applications of vortex lattice theory to preliminary aerodynamic design [PDF]

open access: yes
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.
core   +1 more source

Tip aerodynamics from wind tunnel test of semi-span wing [PDF]

open access: yes
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.
core   +1 more source

Effects of Angle of Attack, Aspect Ratio, and Leading-Edge Curvature on Supersonic Fin Performance

open access: yesAndalasian International Journal of Applied Science, Engineering, and Technology
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
doaj   +1 more source

An aerodynamic study of scramjet fuel injectors [PDF]

open access: yes
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.
core   +1 more source

AERODYNAMIC DRAG AND STABILITY CHARACTERISTICS OF TOWED INFLATABLE DECELERATORS AT SUPERSONIC SPEEDS [PDF]

open access: yes
Aerodynamic drag and stability of towed inflatable decelerators at supersonic ...
Mc Shera, J. T., Jr.
core   +1 more source

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