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Generalized Advanced Propeller Analysis System (GAPAS). Volume 2: Computer program user manualThe Generalized Advanced Propeller Analysis System (GAPAS) computer code is described. GAPAS was developed to analyze advanced technology multi-bladed propellers which operate on aircraft with speeds up to Mach 0.8 and altitudes up to 40,000 feet. GAPAS includes technology for analyzing aerodynamic, structural, and acoustic performance of propellers. The computer code was developed for the CDC 7600 computer and is currently available for industrial use on the NASA Langley computer. A description of all the analytical models incorporated in GAPAS is included. Sample calculations are also described as well as users requirements for modifying the analysis system. Computer system core requirements and running times are also discussed.
Document ID
19900020078
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glatt, L.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Crawford, D. R.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Kosmatka, J. B.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Swigart, R. J.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Wong, E. W.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-185277
NAS 1.26:185277
Report Number: NASA-CR-185277
Report Number: NAS 1.26:185277
Accession Number
90N29394
Funding Number(s)
CONTRACT_GRANT: NAS3-22251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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