Results 111 to 120 of about 10,150 (210)

Exploratory wind-tunnel investigation at high subsonic and transonic speeds of jet flaps on unswept rectangular wings

, 1958
Vernard E Lockwood, Raymond D Vogler
openalex   +1 more source

Computational wing optimization and comparisons with experiment for a semi-span wing model [PDF]

A computational wing optimization procedure was developed and verified by an experimental investigation of a semi-span variable camber wing model in the NASA Ames Research Center 14 foot transonic wind tunnel. The Bailey-Ballhaus transonic potential flow
Ballhaus, W. F., Haney, H. P., Waggoner, E. G.   +2 more
core   +1 more source

Current status and prospects of computer vision-based attitude and deformation measurement applications in wind tunnels. [PDF]

Sci Rep
Xiangyi X, Shuai W, Xu C, Jiang Z, Fanwu M.   +4 more
europepmc   +1 more source

Wind Tunnel Investigation of Passive Vortex Control and Vortex-Tail Interactions on a Slender Wing at Subsonic and Transonic Speeds

, 2013
Gary E. Erickson
openalex   +1 more source

Cryogenic wind tunnels for high Reynolds number testing [PDF]

A compilation of lectures presented at various Universities over a span of several years is discussed. A central theme of these lectures has been to present the research facility in terms of the service it provides to, and its potential effect on, the ...
Kilgore, R. A., Lawing, P. L., Mcguire, P. D.   +2 more
core   +1 more source

Computational fluid dynamics analysis of aerodynamic characteristics in long-endurance unmanned aerial vehicles. [PDF]

Heliyon
Liao Y, Cheng K, Sun W, Zhao Y, Jia X, Qi W.   +5 more
europepmc   +1 more source

A Dynamic Imaging Simulation Method of Infrared Aero-Optical Effect Based on Continuously Varying Gaussian Superposition Model. [PDF]

Sensors (Basel), 2022
Zhang S, Chen X, Zu Y, Rao P.
europepmc   +1 more source

A Study of Subsonic,Two-Dimensional Wall-Interference Effects in a Perforated Wind Tunnel with Particular Reference to the NAL 2m×2m Transonic Wind Tunnel-Inapplicability of the Conventional Boundary Condition

, 1972
Masao Ebihara
openalex   +1 more source

Passive control of suddenly expanded flow and temperature distribution along the duct at critical Mach number. [PDF]

Sci Rep
Tamboli S, Bellary SAI, Abdullah R, Monis RS, Khan SA, Jatti VS, Kate AM, Ingole YR, Jilani SS.   +8 more
europepmc   +1 more source

Optimization of positional parameters of close-formation flight for blended-wing-body configuration. [PDF]

Heliyon, 2018
Yang T, Zhiyong L, Neng X, Yan S, Jun L.
europepmc   +1 more source