Modal Correction Method For Dynamically Induced Errors In Wind-Tunnel Model Attitude Measurements

Modal Correction Method For Dynamically Induced Errors In Wind-Tunnel Model Attitude Measurements

Author(s):

Buehrle, R. D. ( NASA Langley Research Center )
Young, C. P., Jr. ( North Carolina Univ. )

Publication title:

NASA Technical Reports

Pub. Year:

1995

Vol.:

19960025275

Issue:

NASA-TM-111560

Pt.:

NAS 1.15:111560

Paper no.:

N96-27348

Page(from):

1

Page(to):

14

Pages:

14

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001432

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