Results 91 to 100 of about 789,848 (154)

Hypersonic turbulent quantities in support of Morkovin's hypothesis. [PDF]

Nat Commun
Segall BA, Keenoy TC, Kokinakos JC, Langhorn JD, Hameed A, Shekhtman D, Parziale NJ.   +6 more
europepmc   +1 more source

Experimental study of nose-tip bluntness effects on hypersonic boundary-layer transition in a shock tunnel. [PDF]

Sci Rep
Kim J, Nam J, Hur J, Kim J, Lee BJ.
europepmc   +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

Metamaterials and Fluid Flows. [PDF]

Nat Commun
Avallone F, Bosia F, Chen Y, Colombo G, Craster R, De Ponti JM, Fabbiane N, Haberman MR, Hussein MI, Hwang W, Iemma U, Juhl A, Kadic M, Kotsonis M, Laude V, Marquet O, Mery F, Michelis T, Nouh M, Ragni D, Touboul M, Wegener M, Krushynska AO.   +22 more
europepmc   +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

Automated Learning of a Dense Manifold of Electronic States and Electronic Energy Transfer and Reactions in Singlet O Collisions with N₂. [PDF]

Research (Wash D C)
Meng Q, Shu Y, Varga Z, Zhang D, Truhlar DG.   +4 more
europepmc   +1 more source

Research progress on high-enthalpy and hypersonic flows

, 2007
The research progress on high-enthalpy and hypersorlic flows having been achieved in the Institute of Mechanics, Chinese Academy of Sciences, is reported in this paper.
姜宗林, Jiang Z, 林贞彬, 俞鸿儒
core  

Ab initio investigation of a hypersonic double cone experiment. [PDF]

Sci Adv
Grover MS, Valentini P, Bisek N.
europepmc   +1 more source

Influence of Flow Field on the Imaging Quality of Star Sensors for Hypersonic Vehicles in near Space. [PDF]

Sensors (Basel)
Wu S, Sun T, Xing F, Liu H, Yang K, Song J, Yu S, Zhu L.   +7 more
europepmc   +1 more source

Influence of injection angles on flow structures and mixing properties in a supersonic combustor at low Mach supersonic crossflow. [PDF]

Sci Rep
Zhang L, Liang J, Wang Y, Zhao W, Yang L.   +4 more
europepmc   +1 more source