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EFFECTS OF INLET-GUIDE-VANE CONFIGURATION AND RELATIVE BLADE VELOCITY ON NOISE FROM AXIAL-FLOW COMPRESSORS (Record no. 398352)

000 -LEADER
fixed length control field 00439pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number NASA
Item number TN D-5507
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Chestnutt,David
245 1# - TITLE STATEMENT
Title EFFECTS OF INLET-GUIDE-VANE CONFIGURATION AND RELATIVE BLADE VELOCITY ON NOISE FROM AXIAL-FLOW COMPRESSORS
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc. Nasa, Washington, D.C.
Date of publication, distribution, etc. 1969
300 ## - PHYSICAL DESCRIPTION
Extent 25
500 ## - GENERAL NOTE
General note Bound With Nasa Tn D-5500-5506
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Clark,Lorenzo R
964 ## -
-- CIRC
997 ## -
-- TR13687 C
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Full call number Barcode Date last seen Price effective from Koha item type
    Untraceable   General Stacks PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2007-08-12 NASA TN D-5507 TR13687 2016-05-19 2016-05-19 Technical Report

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