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EXPERIMENTAL EVALUATION OF TURNING VANE DESIGNS FOR HIGH-SPEED AND COUPLED FAN-DRIVE CORNERS OF 0.1-SCALE MODEL OF NASA LEWIS RESEARCH CENTER'S PROPOSED ALTITUDE WIND TUNNEL

Author(s):
Gelder, Thomas F. et al. ( NASA )  
Publication title:
NASA Technical Reports(N88-)
Pub. Year:
1987
Issue:
NASA-TP-2681
No.:
H1/09 0124883
Pt.:
NAS1.60:2681
Paper no.:
N88-17686
Page(from):
1
Page(to):
54
Pages:
54
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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