The use of hot-film technique for boundary layer studies on a 21% thick airfoil = Utilisation de la technique du film chaud pour des études de couche limite autour d'un profil d'aile d'une épaisseur relative de 21% /

Bibliographic Details

Main Author:	Khalid, M.
Corporate Authors:	National Research Council of Canada, National Aeronautical Establishment (Canada)
Format:	Book
Language:	English French
Language Notes:	English and French.
Published:	Ottawa : National Research Council Canada, 1987.
Series:	Aeronautical note : no. 45.
Subjects:	Aerofoils. Boundary layer. Aerofoils Boundary layer Airfoils. Boundary layer flow. Hot-film anemometers. Transonic speed.