An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages /

Bibliographic Details

Main Author:	Wang, Tie-cheng
Corporate Authors:	SCITRAN (Firm), United States. National Aeronautics and Space Administration
Format:	Government Document eBook
Language:	English
Published:	Washington DC : National Aeronautics and Space Administration, [1986]
Series:	NASA technical memorandum ; 88385.
Subjects:	Airfoils. Boundary layer transition. Hot-film anemometers. Turbulent boundary layer. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo10972