Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /

Bibliographic Details
Main Author: Hall, Ian Murray
Other Authors: Rogers, E. W. E.
Format: Book
Language:English
Published: London : Her Majesty's Stationery Office, 1962.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3271.
Subjects:

MARC

Tag First Indicator Second Indicator Subfields
LEADER 00000cam a2200000 4500
001 in00000093735
005 20150927070215.0
008 800404s1962 enka b f00010 eng d
035 |a (OCoLC)06169142 
035 |9 AAL5584AM 
040 |a TXA  |c TXA  |d UtOrBLW 
049 |a TXAM  |c [1126980] 
090 |a TL526.G7  |b A4 no. 3271 
100 1 |a Hall, Ian Murray. 
245 1 0 |a Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /  |c by I. M. Hall and E. W. E. Rogers. 
264 1 |a London :  |b Her Majesty's Stationery Office,  |c 1962. 
300 |a 159 pages :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a unmediated  |b n  |2 rdamedia 
338 |a volume  |b nc  |2 rdacarrier 
490 1 |a [Great Britain] Aeronautical Research Council. Reports and memoranda,  |v no. 3271 
500 |a Cover title. 
504 |a Bibliography: pages 10-11, pages 68-70. 
650 0 |a Airplanes  |x Wings, Swept-back. 
650 0 |a Air flow. 
650 0 |a Aerodynamics. 
700 1 |a Rogers, E. W. E. 
830 0 |a Reports and memoranda (Aeronautical Research Council (Great Britain)) ;  |v no. 3271. 
999 |a MARS 
999 f f |s 50dca7ca-c973-316f-9b88-fcdda064b2ae  |i aac469c4-6d68-36bf-a1b0-43085f038a42  |t 0 
952 f f |p ric  |a Texas A&M University  |b Rellis Campus  |c Joint Library Facility  |d Remote Storage  |t 0  |e TL526.G7 A4 no. 3271  |h Library of Congress classification  |i unmediated -- volume  |m A14805535502 
998 f f |a TL526.G7 A4 no. 3271  |t 0  |l Remote Storage