NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Optimization of Air-Breathing Propulsion Engine ConceptsAir-breathing propulsion engines play an important role in the development of both civil and military aircraft Design optimization of such engines can lead to higher power, or more thrust for less fuel consumption. A multimission propulsion engine design can be modeled mathematically as a multivariable global optimization problem, with a sequence of subproblems, which are specific to the mission events defined through Mach number, altitude, and power setting combinations.
Document ID
19970026136
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Patnaik, Surya N.
(Ohio Aerospace Inst. Brook Park, OH United States)
Hopkins, Dale A.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 17, 2013
Publication Date
April 1, 1997
Publication Information
Publication: Physics and Process Modeling (PPM) and Other Propulsion R and T
Volume: 2
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Paper-26
Accession Number
97N25484
Funding Number(s)
CONTRACT_GRANT: NCC3-453
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available