NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A numerical model for dynamic wave rotor analysisA numerical model has been developed which can predict the dynamic (and steady state) performance of a wave rotor, given the geometry and time dependent boundary conditions. The one-dimensional, perfect gas, CFD based code tracks the gasdynamics in each of the wave rotor passages as they rotate past the various ducts. The model can operate both on and off-design, allowing dynamic behavior to be studied throughout the operating range of the wave rotor. The model accounts for several major loss mechanisms including finite passage opening time, fluid friction, heat transfer to and from the passage walls, and leakage to and from the passage ends. In addition, it can calculate the amount of work transferred to and from the fluid when the flow in the ducts is not aligned with the passages such as occurs in off-design operation. Since it is one-dimensional, the model runs reasonably fast on a typical workstation. This paper will describe the model and present the results of some transient calculations for a conceptual four port wave rotor designed as a topping cycle for a small gas turbine engine.
Document ID
19950024196
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Paxson, D. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1995
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:106997
NASA-TM-106997
E-9776
AIAA PAPER 95-2800
Report Number: NAS 1.15:106997
Report Number: NASA-TM-106997
Report Number: E-9776
Report Number: AIAA PAPER 95-2800
Meeting Information
Meeting: AIAA, ASME, SAE, and ASEE
Country: US
Start Date: July 10, 1995
End Date: July 12, 1995
Accession Number
95N30617
Funding Number(s)
PROJECT: RTOP 505-62-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available