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40 396 (0,17s)

Result

Interaction of Supersonic Flows in an Ejector

The paper deals with experimental, theoretical and numerical study of the interaction of supersonic flows on the trailing edge of the primary flow nozzle of a supersonic ejector. Recommendation for design and for o...

BK - Mechanika tekutin

  • 2004
  • D
Result

Interaction of Supersonic Flows in an Ejector

The paper deals with experimental, theoretical and numerical study of the interaction of supersonic flows on the trailing edge of the primary flow nozzle of a supersonic ejector. Recommendations for design and for ...

BK - Mechanika tekutin

  • 2004
  • D
Result

Interaction of supersonic flows in an ejector

The article deals with experimental, theoretical and numerical study of the interaction of supersonic flows in an ejector.

BK - Mechanika tekutin

  • 2005
  • C
Result

Theoretical Research of Supersonic Flow Structure in the Entrance Part of the Mixing Chamber of 2D Ejector

The paper deals with theoretical calculation of supersonic flow structure in the entrance part the mixing chamber of 2D ejector. The results are compared with results of experimental research....

BK - Mechanika tekutin

  • 2002
  • D
Result

On Wakes in an Asymmetric Supersonic Flow Past Trailing Edges of a Profile Blade Cascade

Paper is concerned with results of research on the asymmetric supersonic flow past trailing edge. Distributions of the exit flow angle are compared to theoretical and reference value....

BK - Mechanika tekutin

  • 2009
  • D
Result

Flow Structure in the Mixing Chamber of an Experimental Model of a Supersonic Jet

The experimental data of supersonic flow past the model ejector are presented and analysed.

BK - Mechanika tekutin

  • 2003
  • D
Result

Interaction of supersonic flows in an ejector

of the interaction of supersonic flows on the trailing edge of a primary flow nozzle of an ejector. The mechanism of mutual deflection of supersonic flows is explained. The influences oback pressure ratio...

BK - Mechanika tekutin

  • 2004
  • D
Result

Problematic of instability of supersonic inlet flow field in cascades of tip sections of rotor blades

The paper deals with supersonic flow field instability, which occurs in inlet parts of blade cascades representing tip sections of ultra long rotor turbine blades with supersonic inlet velocities....

BK - Mechanika tekutin

  • 2016
  • D
Result

Verification of K-? SST turbulence model for supersonic internal flows

solver available for the problems in the field of supersonic internal flows. We used the supersonic air-to-air ejector to represent the typical problem in focus interacting in the supersonic ejector making this de...

BK - Mechanika tekutin

  • 2011
  • Jx
  • Link
Result

Experimental Technique for Setup of Supersonic Inlet Flow in a Profile Blade Cascade

The paper deals with methodical approach to investigation of profile blade cascades at supersonic inlet flow conditions. High-speed aerodynamic theory describes inlet supersonic conditions by means of unique incidence rule....

BK - Mechanika tekutin

  • 2014
  • D
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