Boundary layer and wake investigation in supersonic flow / by J. Lukasiewicz and J.K. Royle.

Describes the results of traverses of the boundary layer and wake encountered in a small supersonic tunnel at a Mach number of 2.5.

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Bibliographic Details
Online Access: Online Access
Main Author: Lukasiewicz, J.
Corporate Author: Aeronautical Research Council (Great Britain)
Other Authors: Royle, J. K.
Format: Book
Language:English
Published: London : H.M.S.O, 1952.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 2613.
A.R.C. technical report.
Subjects:

MARC

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245 1 0 |a Boundary layer and wake investigation in supersonic flow /  |c by J. Lukasiewicz and J.K. Royle. 
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300 |a 22 pages :  |b illustrations ;  |c 31 cm. 
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490 1 |a Reports and memoranda / Ministry of Supply, Aeronautical Research Council ;  |v no. 2613 (12,130) 
490 1 |a A.R.C. technical report. 
500 |a "October, 1948" 
500 |a "R.A.E. Report Aero. 2292. S.D.31. Received 3rd February, 1949." 
504 |a Includes bibliographical references (page 9) 
530 |a Also freely available online. 
520 |a Describes the results of traverses of the boundary layer and wake encountered in a small supersonic tunnel at a Mach number of 2.5. 
650 0 |a Aerodynamics, Supersonic.  |0 http://id.loc.gov/authorities/subjects/sh85001297. 
650 0 |a Supersonic wind tunnels.  |0 http://id.loc.gov/authorities/subjects/sh85130657. 
650 0 |a Wall pressure (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85144916. 
650 0 |a Wakes (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85144853. 
700 1 |a Royle, J. K. 
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