NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
The relation between spanwise variations in the critical Mach number and spanwise load distributions
Document ID
19930092722
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Whitcomb, Richard T
Date Acquired
September 6, 2013
Publication Date
December 1, 1944
Report/Patent Number
NACA-WR-L-182
NACA-CB-L4L07
Report Number: NACA-WR-L-182
Report Number: NACA-CB-L4L07
Accession Number
93R22012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOAD DISTRIBUTION, WING-SPAN - TAPERED
AIRFOILS - BOEING 117
AIRFOILS - NACA 23015-4412
AIRFOILS - NACA 63 (420)-422- 63 (420)-517 LOW-DRAG
MACH NUMBER

Related Records

There are no records associated with this record.
No Preview Available