The use of hot-film technique for boundary layer studies on a 21% thick airfoil
By: M. Khalid.
Contributors: National Aeronautical Establishment (Canada)
Series: Aeronautical note -- NAE-AN-45
Publisher: National Aeronautical Establishment
Published: 1987
Place of publication: Ottawa
Number of pages: 46
Subjects: Airfoils; Boundary layer flow; Hot-film anemometers; Transonic speed
Notes: Bibliographical references: p.14-16.