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
Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat
Document ID
19930082391
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Olson, Roland E
Land, Norman S
Date Acquired
August 29, 2013
Publication Date
September 1, 1948
Report/Patent Number
NACA-TN-1571
Report Number: NACA-TN-1571
Accession Number
93R11681
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HULL KEELS - ANGLE OF AFTERBODY
TAKE-OFF & LANDING - FLYING BOATS
TANK TEST (NACA-#1)
HULL AFTERBODIES
STABILITY - FLYING BOATS
HULL STEPS - DEPTH
HULLS - NACA 134A - CHARACTERISTICS

Related Records

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