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Load and dynamic assessment of B-52B-008 carrier aircraft for finned configuration 1 space shuttle solid rocket booster decelerator subsystem drop test vehicle. Volume 2: Airplane flutter and load analysis resultsThe airplane flutter and maneuver-gust load analysis results obtained during B-52B drop test vehicle configuration (with fins) evaluation are presented. These data are presented as supplementary data to that given in Volume 1 of this document. A brief mathematical description of airspeed notation and gust load factor criteria are provided as a help to the user. References are defined which provide mathematical description of the airplane flutter and load analysis techniques. Air-speed-load factor diagrams are provided for the airplane weight configurations reanalyzed for finned drop test vehicle configuration.
Document ID
19790001878
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Quade, D. A. (Boeing Co. Wichita, KS, United States)
Date Acquired
September 3, 2013
Publication Date
June 9, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
D3-11220-2-VOL-2
NASA-CR-150834
Accession Number
79N10049
Funding Number(s)
CONTRACT_GRANT: NAS8-31805
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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