Ejector refrigeration: A comprehensive review

G Besagni, R Mereu, F Inzoli - Renewable and Sustainable Energy …, 2016 - Elsevier
The increasing need for thermal comfort has led to a rapid increase in the use of cooling
systems and, consequently, electricity demand for air-conditioning systems in buildings …

Overview of PIV in supersonic flows

F Scarano - Particle Image Velocimetry: New Developments and …, 2007 - Springer
The extension of particle image velocimetry to supersonic and hypersonic wind-tunnel flows
has been achieved in the last decade. This was mainly possible with the advent of short …

[图书][B] Turbulent shear layers in supersonic flow

AJ Smits, JP Dussauge - 2006 - books.google.com
A good understanding of turbulent compressible flows is essential to the design and
operation of high-speed vehicles. Such flows occur, for example, in the external flow over …

Large-scale structure and entrainment in the supersonic mixing layer

NT Clemens, MG Mungal - Journal of fluid mechanics, 1995 - cambridge.org
Experiments were conducted in a two-stream planar mixing layer at convective Mach
numbers, Mc, of 0.28, 0.42, 0.50, 0.62 and 0.79. Planar laser Mie scattering (PLMS) from a …

Combustion instability of a lean premixed prevaporized gas turbine combustor studied using phase-averaged PIV

JE Temme, PM Allison, JF Driscoll - Combustion and Flame, 2014 - Elsevier
A strong, naturally-occurring “growl” combustion instability was studied for the case of a lean
premixed prevaporized (LPP) combustor that shows great promise in reducing pollutant …

Unsteady aspects of lean premixed prevaporized gas turbine combustors: flame-flame interactions

SK Dhanuka, JE Temme, JF Driscoll - Journal of Propulsion and Power, 2011 - arc.aiaa.org
This work quantifies several sources of unsteadiness that exist within a lean premixed
prevaporized gas turbine combustor that was operated at elevated pressures using Jet-A …

Counterflow thrust vectoring of supersonic jets

PJ Strykowski, A Krothapalli, DJ Forliti - AIAA journal, 1996 - arc.aiaa.org
Nomenclature ai= sound speed in primary stream a2= sound speed in secondary stream C=
transverse collar height CT= thrust coefficient G= counterflow gap height H= short exit …

Novel supersonic nozzles for mixing enhancement in supersonic ejectors

SMV Rao, G Jagadeesh - Applied Thermal Engineering, 2014 - Elsevier
Two novel supersonic nozzles–Tip Ring Supersonic Nozzle and Elliptic Sharp Tipped
Shallow (ESTS) Lobed Nozzle have been developed to enhance mixing at high speeds …

Triggering shock wave positions by patterned energy deposition

P Andrews, P Lax, S Leonov - Energies, 2022 - mdpi.com
The problem considered in this work is shock wave (SW) positioning control in shock-
dominated flows. Experiments are conducted to investigate the triggering effect of patterned …

Flow visualization in supersonic ejectors using laser tomography techniques

A Bouhanguel, P Desevaux, E Gavignet - International journal of …, 2011 - Elsevier
This paper presents flow imaging techniques developed for investigating flow in ejectors.
These visualization techniques use the laser sheet method but differ from each other by the …