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A computer program to generate equations of motion matrices, L217 (EOM). Volume 2: Supplemental system design and maintenance documentThe equations of motion program L217 (EOM) is described. The program formulates the matrix coefficients for a second order linear differential equation which describes the motion of an airplane relative to its level equilibrium flight condition. Aerodynamic data from FLEXSTAB or Doublet Lattice (L216) programs are used to derive the equations for quasi-steady or complete unsteady aerodynamics.
Document ID
19790024995
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clemmons, R. E.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Kroll, R. I.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1979
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
D6-44461-VOL-2
NASA-CR-2852
Report Number: D6-44461-VOL-2
Report Number: NASA-CR-2852
Accession Number
79N33166
Funding Number(s)
CONTRACT_GRANT: NAS1-13918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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