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Calculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634] (Record no. 564090)

000 -LEADER
fixed length control field 00603nam a22001697a 4500
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20210216124012.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 210216b xxu||||| |||| 00| 0 eng d
040 ## - CATALOGING SOURCE
Transcribing agency IIT Kanpur
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title eng
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name Allen,H.Julian
245 ## - TITLE STATEMENT
Title Calculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634]
Statement of responsibility, etc H.Julian Allen
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication Washington,D.C.
Name of publisher National Advisory Committee For Aeronautics
Year of publication 1938
300 ## - PHYSICAL DESCRIPTION
Number of Pages 16p.
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title National Advisory Committee For Aeronautics(NACA)
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Calculation
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Reference
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Accession Number Koha item type
      Reference COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2021-02-16 69740[R.No.634] Technical Report

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