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

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