NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Preliminary Results of Heat Transfer from a Stationary and Rotating Ellipsoidal SpinnerConvective heat-transfer coefficients in dry air were obtained for an ellipsoidal spinner of 30-inch maximum diameter for both stationary and rotating operation over a range of conditions including airspeeds up to 275 miles per hour, rotational speeds up to 1200 rpm, and angles of attack of zero and 40 The results are presented in terms of Nusselt numbers, Reynolds numbers, and convective heat-transfer coefficients. The studies included both uniform heating densities over the spinner and uniform surface temperatures.. In general, the results showed that rotation will increase the convective heat transfer from a spinner, especially in the turbulent-flow regions. Rotation of the spinner at 1200 rpm and at a free-stream velocity of 275 miles per hour increased the Nusselt number parameter in the turbulent-flow region by 32 percent over that obtained with a stationary spinner; whereas in the nose region, where the flow was laminar, an increase of only 18 percent was observed. Transition from laminar to turbulent flow occurred over a large range of Reynolds numbers primarily because of surface roughness of the spinner. Operation at an angle of attack of 40 had only small effects on the local convective heat transfer for the model studied.
Document ID
19810068726
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
vonGlahn, U.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
August 6, 1953
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NACA-RM-E53F02
Accession Number
81N73148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available