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Capabilities and applications of a computer program system for dynamic loads analyses of flexible airplanes with active controls /DYLOFLEX/This paper describes and illustrates the capabilities of the DYLOFLEX Computer Program System. DYLOFLEX is an integrated system of computer programs for calculating dynamic loads of flexible airplanes with active control systems. A brief discussion of the engineering formulation for each of the nine DYLOFLEX programs is described. The capabilities of the system are illustrated by the analyses of two example configurations.
Document ID
19790045002
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Perry, B., III
(NASA Langley Research Center Hampton, VA, United States)
Goetz, R. C.
(NASA Langley Research Center Hampton, Va., United States)
Kroll, R. I.
(Boeing Commercial Airplane Co. Seattle, Wash., United States)
Miller, R. D.
(Boeing Engineering and Construction Co. Seattle, Wash., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 79-0743
Meeting Information
Meeting: Structures, Structural Dynamics, and Materials Conference
Location: St. Louis, MO
Start Date: April 4, 1979
End Date: April 6, 1979
Accession Number
79A29015
Funding Number(s)
CONTRACT_GRANT: NAS1-13918
Distribution Limits
Public
Copyright
Other

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