Parallel effects of acceleration and surface heating on compressible flow: Simulation of an aerospace propulsion nozzle with a medium amount of surface wear

Strojniski Vestnik/Journal of Mechanical Engineering

Volumn 53, Issue 1, 2007, Pages 3-12

  Ozalp, A Alper ^a  

^a ULUDAG UNIVERSITY   (Turkey)

Author keywords

Compressible flow; Discharge coefficient; Power losses; Propulsion nozzle

Indexed keywords

ACCELERATION; AIRCRAFT PROPULSION; BOUNDARY CONDITIONS; DISCHARGE (FLUID MECHANICS); HEAT TRANSFER; NOZZLES; SURFACE ROUGHNESS;

COMPUTATIONAL MODELS; DISCHARGE COEFFICIENT; POWER LOSSES; PROPULSION NOZZLE;

COMPRESSIBLE FLOW;

EID: 34247549794     PISSN: 00392480     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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