Modelling aspects of isentropic compressible gas flow using hydraulic analogy are discussed. Subsonic and supersonic flows through a typical nozzle are simulated as free surface incompressible water flow in an equivalent 2-D model on a water table. The results are first compared for the well known classical analogy in order to estimate experimental errors. Correction factors for pressure and temperature, to account for non-ideal compressible gas flow are presented and the results obtained on the water table are modified and compared with gas dynamic solution. Within the experimental errors, it is shown that the hydraulic analogy can be used as an effective tool for the study of two dimensional isentropic flows of gases
The development of nozzles for hypersonic aircraft is discussed. The simulation of actual nozzle flo...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
Abstract This paper examines the shock cell structure, vorticity and velocity field at the exit of a...
Modelling aspects of isentropic compressible gas flow using hydraulic analogy are discussed. Subsoni...
The theory of hydraulic analogy, that is, the analogy between water flow with a free surface and two...
The theory of ~ke hydraulic analogy—tha ~ is, the analogy betuwn water jimo m“th a free surface and ...
The theory of the hydraulic analogy -- that is, the analogy between water flow with a free surface a...
A water channel was constructed and calibrated in order to carry out tests on a supersonic perforate...
The theory of the hydraulic jump is presented briefly, and the analogy between this phenomenon and t...
Determination of non-steady forces in a real turbine stage is difficult due to the local flow condit...
The present work studies the hydro-gasdynamic analogy between a shock wave, occurring in supersonic ...
The present work depicts the development of an experimental equipment that reveals compressible flui...
It has been known for some time that an analogy exists between t he flow of a liquid with a free sur...
Experiments were performed on equivalent two-dimensional axi-symmetric combustor model using modifie...
This paper examines the shock cell structure at the exit of an underexpanded jet nozzle using a hydr...
The development of nozzles for hypersonic aircraft is discussed. The simulation of actual nozzle flo...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
Abstract This paper examines the shock cell structure, vorticity and velocity field at the exit of a...
Modelling aspects of isentropic compressible gas flow using hydraulic analogy are discussed. Subsoni...
The theory of hydraulic analogy, that is, the analogy between water flow with a free surface and two...
The theory of ~ke hydraulic analogy—tha ~ is, the analogy betuwn water jimo m“th a free surface and ...
The theory of the hydraulic analogy -- that is, the analogy between water flow with a free surface a...
A water channel was constructed and calibrated in order to carry out tests on a supersonic perforate...
The theory of the hydraulic jump is presented briefly, and the analogy between this phenomenon and t...
Determination of non-steady forces in a real turbine stage is difficult due to the local flow condit...
The present work studies the hydro-gasdynamic analogy between a shock wave, occurring in supersonic ...
The present work depicts the development of an experimental equipment that reveals compressible flui...
It has been known for some time that an analogy exists between t he flow of a liquid with a free sur...
Experiments were performed on equivalent two-dimensional axi-symmetric combustor model using modifie...
This paper examines the shock cell structure at the exit of an underexpanded jet nozzle using a hydr...
The development of nozzles for hypersonic aircraft is discussed. The simulation of actual nozzle flo...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
Abstract This paper examines the shock cell structure, vorticity and velocity field at the exit of a...