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Effect of Structural Flexibility on the Design of Vibration-Isolating Mounts for Aircraft Engines

Author(s):
Philips, W. H. ( Langley Research center )  
Publication title:
NASA Technical Reports
Pub. Year:
1984
Issue:
NASA-TM-85725
No.:
G3/39 18216
Pt.:
NAS 1.15:85725
Paper no.:
N84-16590
Page(from):
1
Page(to):
24
Pages:
24
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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