NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of NACA Injection Impeller and Ducted Head Baffles on Flight Cooling Performance of Double-row Radial Engine in Four-engine Heavy Bomber
Document ID
19930093216
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Vensel, Joseph R
Date Acquired
September 6, 2013
Publication Date
April 1, 1945
Report/Patent Number
NACA-MR-E5D13
NACA-WR-E-256
Accession Number
93R22506
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ENGINES-WRIGHT R-3350 (AMER )
COOLING TESTS
FLIGHT TESTS
COOLING SYSTEMS-BOEING B-29
IMPELLERS, FUEL-INJECTION-NACA
BAFFLES-ENGINE CYLINDERS
No Preview Available