NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

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
Report Number: NACA-MR-E5D13
Report Number: 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