Results 121 to 130 of about 74,712 (235)

Isogeometric analysis of wing structures using multipatch parametrization and penalty-based coupling method. [PDF]

Sci Rep
Wang D, Cao X, Xue Y, Wang W, Du X.
europepmc   +1 more source

Supersonic aeroelastic instability results for a NASP-like wing model [PDF]

An experimental study and an analytical study have been conducted to examine static divergence for hypersonic-vehicle wing models at supersonic conditions.
Bullock, Ellen P., Cole, Stanley R., Florance, James R., Spain, Charles V., Thomason, Lee B.   +4 more
core   +1 more source

Numerical and Experimental Investigation of Thickness Effect on the Cambered Airfoils at Low Reynolds Numbers

Havacılık ve Uzay Teknolojileri Dergisi
In this study, experimentaland numerical study for the cambered airfoils was conducted at Re = 1.5x105and Re = 2.5x105and different angles of attack.
Muhammer Ayvazoğlu, Sinem Keskin, Rümeysa Şahin, Mehmet Sincar, Eren Anıl Sezer, Halil Hakan Açıkel, Mustafa Özden, Mustafa Serdar Genç   +7 more
doaj  

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

Bridging spatial and temporal surface pressure dynamics for gust aerodynamic modeling. [PDF]

Commun Eng
Chen D, Liang A, Sun B, Rival DE, Fan D.
europepmc   +1 more source

Aerodynamic data banks for Clark-Y, NACA 4-digit and NACA 16-series airfoil families [PDF]

With the renewed interest in propellers as means of obtaining thrust and fuel efficiency in addition to the increased utilization of the computer, a significant amount of progress was made in the development of theoretical models to predict the ...
Camba, J., III, Korkan, K. D., Morris, P. M.   +2 more
core   +1 more source

Shape Parameterization and Efficient Optimization Design Method for the Ray-like Underwater Gliders. [PDF]

Biomimetics (Basel)
Zhang D, Zeng D, Zhou H, Bao C, Liu Q.
europepmc   +1 more source

Transonic flow past an airfoil with condensation [PDF]

In connection with investigations conducted to determine the influence of water vapor on experiments in wind tunnels, the question arose as to what changes due to vapor condensation might be expected in airfoil measurements.
Schmidt, B.
core   +1 more source

Numerical and experimental investigation on aeroelasticity of wind turbine blade with biological airfoil and V‑stripe web. [PDF]

Sci Rep
Chen K, Ren K, Zhao P, Su T, Hao Z, Wang Q, Zhao Z.   +6 more
europepmc   +1 more source

Solution of transonic flows by an integro-differential equation method [PDF]

Solutions of steady transonic flow past a two-dimensional airfoil are obtained from a singular integro-differential equation which involves a tangential derivative of the perturbation velocity potential.
Ogana, W.
core   +1 more source