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Effects of Vibration on Inertial Wind-Tunnel Model Attitude Measurement Devices

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1994
Issue:
NASA-TM-109063
Pt.:
NAS 1.15:109063
Paper no.:
N95-11466
Page(from):
1
Page(to):
34
Pages:
34
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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