NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 482
Release: 1974
Genre:
ISBN:

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Total Pages: 472
Release:
Genre: Aeronautics
ISBN:

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A Selected Listing of NASA Scientific and Technical Reports

A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Total Pages: 470
Release: 1969
Genre: Aeronautics
ISBN:

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Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 814
Release: 1968
Genre: Mechanics, Applied
ISBN:

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Investigation of Flow Separation on a Two-dimensional Flat Plate Haveing a Variable-san Trailing-edge Flap at M [free Stream]

Investigation of Flow Separation on a Two-dimensional Flat Plate Haveing a Variable-san Trailing-edge Flap at M [free Stream]
Author: S. R. Pate
Publisher:
Total Pages: 46
Release: 1964
Genre: Laminar boundary layer
ISBN:

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An experimental investigation of separated boundary-layer flow was conducted on a two-dimensional flat plate having a variable-span trailing edge flap in the 12-in. Supersonic Tunnel (D) of the von Karman Gas Dynamics Facility. The tests were made at Mach numers 3 and 5 at zero angle of attack and over a Reynolds number range (based on plate length) from 0.26 to 16.7 x 10 to the 6th power. Model surface pressure distributions, schlieren photographs, and velocity distributions are presented. The effects of unit Reynolds number, plate length, flap span, and flap deflection angle on the separated region are investigated, and comparisons are made with existing theory.