Publication Date:
2013-08-31
Description:
The purpose is to re-examine the heat transfer from a hot-wire probe in the compressible subsonic flow regime; describe the three-wire hot-wire probe calibration and data reduction techniques used to measure the velocity, density, and total temperature fluctuation; and present flow quality results obtained in the Langley 0.3 meter Transonic Cryogenic Wind Tunnel and in flight with the NASA JetStar from the same three-wire hot-wire probe.
Keywords:
AERODYNAMICS
Type:
Research in Natural Laminar Flow and Laminar-Flow Control, Part 2; p 345-357
Format:
application/pdf