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Analytic methods for design of wave cycles for wave rotor core enginesA procedure to design a preliminary wave rotor cycle for any application is presented. To complete a cycle with heat addition there are two separate but related design steps that must be followed. The 'wave' boundary conditions determine the allowable amount of heat added in any case and the ensuing wave pattern requires certain pressure discharge conditions to allow the process to be made cyclic. This procedure, when applied, gives a first estimate of the cycle performance and the necessary information for the next step in the design process, namely the application of a characteristic based or other appropriate detailed one dimensional wave calculation that locates the proper porting around the periphery of the wave rotor. Four examples of the design procedure are given to demonstrate its utility and generality. These examples also illustrate the large gains in performance that could be realized with the use of wave rotor enhanced propulsion cycles.
Document ID
19930066256
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Resler, Edwin L., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Mocsari, Jeffrey C.
(NASA Lewis Research Center Cleveland, OH, United States)
Nalim, M. R.
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-2523
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: SAE, AIAA, ASEE, ASME
Accession Number
93A50253
Distribution Limits
Public
Copyright
Other

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