NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Planing-surface Tests at Large Froude Numbers - Airfoil ComparisonThe take-off capacity of a flying boat depends upon the design of the hull bottom ahead as well as aft of the step. Systematic tests - largely made by industry itself - had proved the benefit accruing from a well designed hull bottom long before theoretical insight into the flow phenomena involved had been obtained. The theoretical framing of the problem was beset with serious difficulties and, though restricted to the processes within range of the planing bottom ahead of the step, the solutions do not yet afford a comprehensive survey.
Document ID
19930094568
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sambraus, A
Date Acquired
September 6, 2013
Publication Date
February 1, 1938
Report/Patent Number
NACA-TM-848
Report Number: NACA-TM-848
Accession Number
93R23488
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available