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DEVELOPMENT AND APPLICATION OF A PROGRAM TO CALCULATE TRANSONIC FLOW AROUND AN OSCILLATING THREE-DIMENSIONAL WING USING FINITE DIFFERENCE PROCEDURES Final Report

Author(s):
Weatherill, Warren H. et al. ( Boeing Commercial Airplane Co. )  
Publication title:
NASA Technical Reports(N89)
Pub. Year:
1989
Issue:
NASA-CR-181744
No.:
G3/02 0190960
Pt.:
NAS1.26:181744
Paper no.:
N89-20093
Page(from):
1
Page(to):
91
Pages:
91
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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