Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment /

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Bibliographic Details
Author / Creator:Abbott, I. H., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1931.
Description:1 online resource (6 pages, 5 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 371
Technical note (United States. National Advisory Committee for Aeronautics) ; 371.
Subject:Boundary layer control.
Aerofoils.
Leading edges (Aerodynamics)
Lift (Aerodynamics)
Angle of attack (Aerodynamics)
Angle of attack (Aerodynamics)
Boundary layer control.
Lift (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12691665
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"April, 1931."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (pages 5-6).
Description based on online resource, PDF version; title from title page (TRAIL, viewed December 4, 2020).
Other form:Print version: Abbott, I.H. Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/371