Results 71 to 80 of about 4,183,596 (242)

Computer program determines gas flow rates in piping systems [PDF]

open access: yes, 1966
Computer program calculates the steady state flow characteristics of an ideal compressible gas in a complex piping system. The program calculates the stagnation and total temperature, static and total pressure, loss factor, and forces on each element in ...
Franke, R.
core   +1 more source

On the influence of the nozzle external configuration on the radiated screech and the decay of supersonic jets

open access: yesArchives of Acoustics, 2016
The behaviour of screeching jets exhausting from an axisymmetric con-vergent-divergent nozzle was studied. The nozzle had a 2.9 mm throat diameter and a. 1.95 theoretical exit Mach number.
Giovanni Maria CARLOMAGNO   +2 more
doaj  

Analysis of flow-field in a dual mode ramjet combustor with boundary layer bleed in isolator

open access: yesPropulsion and Power Research, 2021
A two-dimensional Reynolds averaged Navier Stokes (RANS) simulation of a dual mode ramjet (DMRJ) combustor is performed, modeling the University of Michigan dual-mode combustor experimental setup operating in reacting mode with different equivalence ...
Nishanth Thillai   +3 more
doaj  

Micrometer-sized droplets from liquid helium jets at low stagnation pressures [PDF]

open access: hybrid, 2022
Katharina Kolatzki   +5 more
openalex   +1 more source

Calibration Probe Uncertainty and Validation for the Hypersonic Material Environmental Test System [PDF]

open access: yes
This paper presents an uncertainty analysis of the stagnation-point calibration probe surface predictions for conditions that span the performance envelope of the Hypersonic Materials Environmental Test System facility located at NASA Langley Research ...
Brune, Andrew J.   +2 more
core   +1 more source

Stagnation–saddle points and flow patterns in Stokes flow between contra-rotating cylinders [PDF]

open access: yes, 1998
The steady flow is considered of a Newtonian fluid, of viscosity mu, between contra-rotating cylinders with peripheral speeds U-1 and U-2 The two-dimensional velocity field is determined correct to O(H-0/2R)(1/2), where 2H(0) is the minimum separation of
Gaskell, P.H.   +2 more
core   +1 more source

Analysis and testing of two-dimensional vented Coanda ejectors with asymmetric variable area mixing sections [PDF]

open access: yes
The analysis of asymmetric, curved (Coanda) ejector flow has been completed using a finite difference technique and a quasi-orthogonal streamline coordinate system.
Armstrong, R. L.   +3 more
core   +1 more source

Steady flow over triangular extended solid attached to square cylinder – A method to reduce drag

open access: yesAin Shams Engineering Journal, 2015
Numerical analysis of two dimensional steady flows over a triangular extended solid (thorn) attached to square cylinder positioned at front stagnation point and at rear stagnation point separately is reported at low Reynolds number (Re = 40).
Prasenjit Dey, Ajoy Kr. Das
doaj   +1 more source

Two-phase choked flow of subcooled nitrogen through a slit [PDF]

open access: yes
Two-phase choked flow rate and pressure distribution data are reported for subcooled nitrogen flowing through a slit. The slip was a narrow rectangular passage of equal length and width. The inlet stagnation pressure ranged from slightly above saturation
Simoneau, R. J.
core   +1 more source

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