Results 141 to 150 of about 15,113 (249)

Transonic unsteady airloads on an energy efficient transport wing with oscillating control surfaces [PDF]

An aspect ratio 10.8 supercritical wing with oscillating control surfaces is described. The wing is instrumental with 252 static orifices and 164 in situ dynamic pressure transducers for studying the effects of control surface deflection on steady and ...
Cazier, F. W., Jr., Cunningham, H. J., Ricketts, R. H., Sandford, M. C.   +3 more
core   +1 more source

Weak wall boundary conditions for compressible flows. [PDF]

Eng Comput
Jaiswal M, Rajanna MR, Islam MR, Hsu MC, Bazilevs Y.   +4 more
europepmc   +1 more source

Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing [PDF]

The flow over the B-1 wing is studied computationally, including the aeroelastic response of the wing. Computed results are compared with results from wind tunnel and flight tests for both low-sweep and high-sweep cases, at 25.0 deg.
Goorjian, P. M., Guruswamy, G. P., Ide, H., Miller, G.   +3 more
core   +1 more source

Three-Dimensional Deformation Calculation of Wind Tunnel Flexible Wall Using Orthogonal Beam Function. [PDF]

Materials (Basel)
Yang X, Ma Y, Wang G, Yang C, Yu C.
europepmc   +1 more source

Buffet characteristics of the F-8 supercritical wing airplane [PDF]

The buffet characteristics of the F-8 supercritical wing airplane were investigated. Wing structural response was used to determine the buffet characteristics of the wing and these characteristics are compared with wind tunnel model data and the wing ...
Deangelis, V. M., Monaghan, R. C.
core   +1 more source

Aerodynamic Effects of a Blended Multi-Winglet on an Airliner in Subsonic and Transonic Regimes. [PDF]

Biomimetics (Basel)
Kobayashi E, Chiba K, Yamazaki W, Kanazaki M.   +3 more
europepmc   +1 more source

Numerical study of probe parameters on performance of a transonic axial compressor. [PDF]

PLoS One, 2021
Islam A, Ma H.
europepmc   +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

Measurement of model aeroelastic deformations in the wind tunnel at transonic speeds using stereophotogrammetry [PDF]

A stereophotographic method of determining the aeroelastic deformations of an airplane model under aerodynamic load in the wind tunnel was evaluated. Wind tunnel tests were conducted in the Langley 8 foot transonic pressure tunnel on the wing of a 0.0625
Beamish, J. K., Brooks, J. D.
core   +1 more source

High-Reynolds-Number Turbulence Database: AeroFlowData. [PDF]

Sci Data
Zhang W, Shan X, Liu Y, Zhang X, Wan Z, Li X, Sha X, Zhao J, Xu H, He C, Liu Y, Xia Z, Li W, Gao L, Jin X, Li H, Liao F, Zhang Y, Chen G.   +18 more
europepmc   +1 more source