Ejector refrigeration: A comprehensive review
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 …
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 …
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 …
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 …
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
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 …
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 …
prevaporized gas turbine combustor that was operated at elevated pressures using Jet-A …
Counterflow thrust vectoring of supersonic jets
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 …
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 …
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 …
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 …
These visualization techniques use the laser sheet method but differ from each other by the …