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Computer program to prepare airfoil characteristic data for use in helicopter performance calculationsA computer program developed to prepare wind tunnel generated airfoil data for input into helicopter performance prediction programs is described. The program provides for numerically cross plotting the data, plotting the data, and tabulating and punching the tabulated result into computer cards for use in the rotorcraft flight simulation model.
Document ID
19800006772
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jones, H. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
L-11608
NASA-TM-78627
Accession Number
80N15031
Funding Number(s)
PROJECT: RTOP 505-10-23-03
PROJECT: DA PROJ. 1L1-61102-AH-45
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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