Related Books

Investigation of Drag Reduction by Boundary Layer Suction on a 72.5-deg Swept Wind at M 2 and 2.25
Language: en
Pages: 27
Authors: S. R. Pate
Categories:
Type: BOOK - Published: 1963 - Publisher:

DOWNLOAD EBOOK

Tests were conducted in the 40-Inch Supersonic Tunnel (A) of the von Karman Gas Dynamics Facility to determine the effectiveness of boundary layer suction for l
INVESTIGATION OF DRAG REDUCTION BY BOUNDARY-LAYER SUCTION ON A 36-DEG SWEPT WING AT M
Language: en
Pages: 36
Investigation of Drag Reduction by Boundarylayer Suction on a 50-degree Swept Tapered Wing at M (free-stream) Equals 2.5 to 4
Language: en
Pages: 31
Authors: S. R. Pate
Categories:
Type: BOOK - Published: 1964 - Publisher:

DOWNLOAD EBOOK

Tests were conducted in the 40-in. supersonic Tunnel A of the von Karman Gas Dynamics Facility to determine the effectiveness of boundarylayer suction for lamin
Viscous Drag Reduction
Language: en
Pages: 497
Authors: C. Sinclair Wells
Categories: Technology & Engineering
Type: BOOK - Published: 2013-12-20 - Publisher: Springer

DOWNLOAD EBOOK

Theoretical Investigation of Drag Reduction in Maintaining the Laminar Boundary Layer by Suction
Language: en
Pages: 60
Authors: A. Ulrich
Categories: Boundary layer control
Type: BOOK - Published: 1947 - Publisher:

DOWNLOAD EBOOK

Maintenance of a laminar boundary layer by suction was suggested recently to decrease the friction drag of an immersed body, in particular an airfoil section [1