Results 251 to 260 of about 6,875 (317)

Abundant water from primordial supernovae at cosmic dawn. [PDF]

Nat Astron
Whalen DJ, Latif MA, Jessop C.
europepmc   +1 more source

Online Chemical Analysis of Flowing <i>n</i>-Hexane in a Pyrolysis Reactor by Optical Spectroscopy and Molecular Beam Mass Spectrometry. [PDF]

J Phys Chem A
Rohan MC, VanDyke CJ, Hanchak MS, Craft EM, Kurian ES, Tucker AD, Lewis WK, DeBlase AF.   +7 more
europepmc   +1 more source

Accreting White Dwarfs: An Unreview. [PDF]

Space Sci Rev
Scaringi S, Knigge C, de Martino D.
europepmc   +1 more source

AHKASH: a new Hybrid particle-in-cell code for simulations of astrophysical collisionless plasma. [PDF]

Mon Not R Astron Soc
Achikanath Chirakkara R, Federrath C, Seta A.   +2 more
europepmc   +1 more source

Computational modeling of the rectangular non-aligned multi-injector for efficient fuel mixing in a supersonic combustion chamber. [PDF]

Sci Rep
Zhang P, Li Z, Abdollahi SA.
europepmc   +1 more source

Generation of highly stable electron beam via the control of hydrodynamic instability. [PDF]

Sci Rep
Gu YJ, Jin Z, Lei ZZ, Sato S, Huang K, Nakanii N, Daito I, Kando M, Hosokai T.   +8 more
europepmc   +1 more source

IUTAM Symposium on Combustion in Supersonic Flows proceedings of the IUTAM Symposium held in Poitiers, France, 2 - 6 October 1995

, 1997
Symposium on Combustion in Supersonic Flows 1995 Poitiers, Champion, Michel   +1 more
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Generation of protosnowflakes in supersonic flow

The Journal of Chemical Physics, 2009
Nanocrystals of ice were generated at about 200 K by the freezing of minuscule liquid drops of water produced in supersonic flow by the condensation of supersaturated water vapor. Although the mode of generation differs from that of snowflake nuclei formed in the upper atmosphere, the temperature involved is similar and the corresponding kinetics of ...
Lawrence S, Bartell, Paul J, Lennon
openaire   +2 more sources

The Flow of a Supersonic Jet in a Supersonic Stream at an Angle of Attack

Journal of the Aerospace Sciences, 1958
where M is the Mach Number, P the pressure, and the subscripts, 1 and 2, refer to the jet stream and the exterior flow, respectively. If k = 1, for two dimensions there are no reflections from the jet interface and the jet aligns itself with the original undisturbed flow in a finite distance.
Ehlers, F. Edward, Strand, Torstein
openaire   +2 more sources

Supersonic Nozzle Flow

2022
The nozzle flow is considered to be much more important in aerospace applications. Based on the pressure, velocity and temperature, flow velocity, Mach number and area, the nozzle shape will vary to meet the required condition. Nozzle is a part where the potential energy is converted into kinetic energy.
Nithya Subramani, Manigandan Sekar, Yasin Sohret, Gowtham Gajapathy   +3 more
openaire   +1 more source