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PRESSURE DISTRIBUTIONS FROM HIGH REYNOLDS NUMBER TRANSONIC TESTS OF AN NACA 0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Author(s):
Ladson, Charies L. et al. ( NASA )  
Publication title:
NASA Technical Reports(N88-)
Pub. Year:
1987
Issue:
NASA-TM-100526
No.:
G3/02 0129396
Pt.:
NAS1.15:100526
Paper no.:
N88-18565
Page(from):
1
Page(to):
396
Pages:
396
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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