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Correlation of Mixture Temperature Data Obtained from Bare Intake-manifold ThermocouplesA relatively simple equation has been found to express with fair accuracy, variation in manifold-charge temperature with charge in engine operating conditions. This equation and associated curves have been checked by multi cylinder-engine data, both test stand and flight, over a wide range of operating conditions. Average mixture temperatures, predicted by the equations of this report, agree reasonably well with results within the same range of carburetor-air temperatures from laboratories and test stands other than the NACA.
Document ID
19930093118
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
White, H. Jack
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Gammon, Goldie L
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1946
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-WR-E-273
NACA-MR-E5L03
Report Number: NACA-WR-E-273
Report Number: NACA-MR-E5L03
Accession Number
93R22408
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ENGINES-PRATT & WHITNEY R-1830-75 (AMER )
FUEL-AIR MIXTURES-TEMPERATURES
MANIFOLDS, INTAKE-TEMPERATURES
DETONATION-EFFECT OF MANIFOLD TEMPERATURES
COMMITTEES-NACA-SUBCOM ON AIRCRAFT FUELS & LUBRICANTS (AMER)
ENGINES-PRATT & WHITNEY R-1830-90C (AMER )
ENGINES-PRATT & WHITNEY R-1830-94 (AMER )
FUELS-TRIPTANE
INSTRUMENTS-THERMOCOUPLES
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