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Simplified, inverse, ejector design toolA simple lumped parameter based inverse design tool has been developed which provides flow path geometry and entrainment estimates subject to operational, acoustic, and design constraints. These constraints are manifested through specification of primary mass flow rate or ejector thrust, fully-mixed exit velocity, and static pressure matching. Fundamentally, integral forms of the conservation equations coupled with the specified design constraints are combined to yield an easily invertible linear system in terms of the flow path cross-sectional areas. Entrainment is computed by back substitution. Initial comparison with experimental and analogous one-dimensional methods show good agreement. Thus, this simple inverse design code provides an analytically based, preliminary design tool with direct application to High Speed Civil Transport (HSCT) design studies.
Document ID
19940019038
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dechant, Lawrence J.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
E-8289
NAS 1.26:194438
NASA-CR-194438
Report Number: E-8289
Report Number: NAS 1.26:194438
Report Number: NASA-CR-194438
Accession Number
94N23511
Funding Number(s)
PROJECT: RTOP 505-69-50
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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