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Analysis of Flight-determined and Predicted Effects of Flexibility on the Steady-state Wing Loads of the B-52 AirplaneFlight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplane
Document ID
19660030327
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Kuhl, A. E.
(NASA Flight Research Center Edwards, CA, United States)
Little, M. V.
(NASA Flight Research Center Edwards, CA, United States)
Rogers, J. T.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 23, 1958
Subject Category
Aircraft
Report/Patent Number
NACA-RM-H57C25
Accession Number
66N39617
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING LOADING
FLEXIBILITY
B-52 AIRCRAFT
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