Matches in SemOpenAlex for { <https://semopenalex.org/work/W293443359> ?p ?o ?g. }
Showing items 1 to 84 of
84
with 100 items per page.
- W293443359 abstract "Abstract : The overall objective of the work described herein was to develop an improved method for the computation of the influence of external disturbances on turbine engine compressor stability, and, in so doing, to gain added physical insight into the destabilizing processes. The objectives were accomplished through the development of a one-dimensional, time-dependent mathematical compressor model for analysis of planar disturbances and an extension of the model to a three-dimensional form for analysis of distorted inflows. The models satisfy mass, momentum and energy equations on a time-dependent basis. Compressor stage force and shaft work were determined from empirical stage characteristics with corrections made for unsteady cascade airfoil aerodynamics. The system of equations comprising the model is solved using a digital computer. Example problems with comparisons to experiments are presented for three different compressors. Example problems solved using the one-dimensional analysis include: determination of the steady-state stability limit (surge line) with undisturbed flow, instability caused by oscillating planar inflow, dynamic response of a compressor to oscillating entry pressure, dynamic response to oscillating discharge pressure, and compressor instability caused by rapid upward ramps of entry temperature. Example problems solved using the distortion model include: stability limit (surge) line reduction caused by a combined radial and circumferential pressure distortion, time-variant distortion effects, pure radial pressure distortion effects, and pure pressure and temperature circumferential distortion effects." @default.
- W293443359 created "2016-06-24" @default.
- W293443359 creator A5081846104 @default.
- W293443359 date "1977-08-01" @default.
- W293443359 modified "2023-09-27" @default.
- W293443359 title "An Analysis of the Influence of some External Disturbances on the Aerodynamic Stability of Turbine Engine Axial Flow Fans and Compressors" @default.
- W293443359 hasPublicationYear "1977" @default.
- W293443359 type Work @default.
- W293443359 sameAs 293443359 @default.
- W293443359 citedByCount "12" @default.
- W293443359 countsByYear W2934433592016 @default.
- W293443359 crossrefType "journal-article" @default.
- W293443359 hasAuthorship W293443359A5081846104 @default.
- W293443359 hasConcept C112124176 @default.
- W293443359 hasConcept C119599485 @default.
- W293443359 hasConcept C121332964 @default.
- W293443359 hasConcept C126780896 @default.
- W293443359 hasConcept C127413603 @default.
- W293443359 hasConcept C131097465 @default.
- W293443359 hasConcept C13393347 @default.
- W293443359 hasConcept C154108245 @default.
- W293443359 hasConcept C154945302 @default.
- W293443359 hasConcept C180788929 @default.
- W293443359 hasConcept C194257627 @default.
- W293443359 hasConcept C24326235 @default.
- W293443359 hasConcept C2775924081 @default.
- W293443359 hasConcept C2776132308 @default.
- W293443359 hasConcept C2778449969 @default.
- W293443359 hasConcept C38349280 @default.
- W293443359 hasConcept C41008148 @default.
- W293443359 hasConcept C46362747 @default.
- W293443359 hasConcept C47446073 @default.
- W293443359 hasConcept C57879066 @default.
- W293443359 hasConcept C78519656 @default.
- W293443359 hasConcept C96261405 @default.
- W293443359 hasConceptScore W293443359C112124176 @default.
- W293443359 hasConceptScore W293443359C119599485 @default.
- W293443359 hasConceptScore W293443359C121332964 @default.
- W293443359 hasConceptScore W293443359C126780896 @default.
- W293443359 hasConceptScore W293443359C127413603 @default.
- W293443359 hasConceptScore W293443359C131097465 @default.
- W293443359 hasConceptScore W293443359C13393347 @default.
- W293443359 hasConceptScore W293443359C154108245 @default.
- W293443359 hasConceptScore W293443359C154945302 @default.
- W293443359 hasConceptScore W293443359C180788929 @default.
- W293443359 hasConceptScore W293443359C194257627 @default.
- W293443359 hasConceptScore W293443359C24326235 @default.
- W293443359 hasConceptScore W293443359C2775924081 @default.
- W293443359 hasConceptScore W293443359C2776132308 @default.
- W293443359 hasConceptScore W293443359C2778449969 @default.
- W293443359 hasConceptScore W293443359C38349280 @default.
- W293443359 hasConceptScore W293443359C41008148 @default.
- W293443359 hasConceptScore W293443359C46362747 @default.
- W293443359 hasConceptScore W293443359C47446073 @default.
- W293443359 hasConceptScore W293443359C57879066 @default.
- W293443359 hasConceptScore W293443359C78519656 @default.
- W293443359 hasConceptScore W293443359C96261405 @default.
- W293443359 hasLocation W2934433591 @default.
- W293443359 hasOpenAccess W293443359 @default.
- W293443359 hasPrimaryLocation W2934433591 @default.
- W293443359 hasRelatedWork W1976593235 @default.
- W293443359 hasRelatedWork W2004333647 @default.
- W293443359 hasRelatedWork W2030453229 @default.
- W293443359 hasRelatedWork W2030564862 @default.
- W293443359 hasRelatedWork W2037633716 @default.
- W293443359 hasRelatedWork W2045716808 @default.
- W293443359 hasRelatedWork W2052552702 @default.
- W293443359 hasRelatedWork W2062073777 @default.
- W293443359 hasRelatedWork W2063350602 @default.
- W293443359 hasRelatedWork W2067609267 @default.
- W293443359 hasRelatedWork W2068693448 @default.
- W293443359 hasRelatedWork W2314624145 @default.
- W293443359 hasRelatedWork W2347439064 @default.
- W293443359 hasRelatedWork W2366782960 @default.
- W293443359 hasRelatedWork W2387015218 @default.
- W293443359 hasRelatedWork W2464118806 @default.
- W293443359 hasRelatedWork W2519166510 @default.
- W293443359 hasRelatedWork W2612502625 @default.
- W293443359 hasRelatedWork W3086647939 @default.
- W293443359 hasRelatedWork W849354336 @default.
- W293443359 isParatext "false" @default.
- W293443359 isRetracted "false" @default.
- W293443359 magId "293443359" @default.
- W293443359 workType "article" @default.