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A WIND TUNNEL TEST OF 22% SCALE MODEL OF A WINDMILL WITH A TWO-BLADED ROTOR OF 14m DIAMETER FOR FIELD TEST

Author(s):
Ishida, Y. ( National Aerospace Lab. )  
Publication title:
NASA Technical Reports
Pub. Year:
1985
Issue:
NAL-TR-887
No.:
G6/02 16530
Paper no.:
N86-20367
Page(from):
1
Page(to):
21
Pages:
21
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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