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Comparison Between Flight-measured and Calculated Span Load Distribution at High Mach Numbers
Document ID
19930085791
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rolls, L Stewart
Date Acquired
August 16, 2013
Publication Date
November 26, 1947
Report/Patent Number
NACA-RM-A7G17
Report Number: NACA-RM-A7G17
Accession Number
93R15081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOADS, STEADY AERODYNAMIC - WINGS
MACH NUMBER EFFECTS - COMPLETE WINGS
WINGS, COMPLETE - DESIGN VARIABLES
LOADS, STRUCTURAL, BENDING

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