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Comparison of aerodynamic coefficients obtained from theoretical calculations wind tunnel tests and flight tests data reduction for the alpha jet aircraft (Record no. 564262)

000 -LEADER
fixed length control field 00848nam a22001697a 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20210304165806.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 210304b 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
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number NASA
Item number TM-75237
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name Guiot, R.
245 ## - TITLE STATEMENT
Title Comparison of aerodynamic coefficients obtained from theoretical calculations wind tunnel tests and flight tests data reduction for the alpha jet aircraft
Remainder of title The methods by which aerodynamic coefficients are determined and discussed. These include: calculations, wind tunnel experiments and experiments in flight for various prototypes of the Alpha Jet. A comparison of obtained results shows good correlation between expectations and in-flight test results.
Statement of responsibility, etc R. Guiot and H. Wunnenberg
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term NASA Technical Report
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Wunnenberg, H.
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Full call number Accession Number Koha item type
        COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2021-03-04 NASA TM-75237 A71053 Technical Report

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