use of hot-film technique for boundary layer studies on a 21% thick airfoil
By: by M. Khalid.
Contributors: National Research Council of Canada.; National Aeronautical Establishment (Canada)
Series: National Research Council Canada -- 27892; Aeronautical Note / National Aeronautical Establishment -- AN45
Publisher: NationalResearch Council Canada
Published: 1987
Place of publication: Ottawa
Language: eng
Number of pages: 46