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LOW SPEED WIND TUNNEL TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 1: TEST

Author(s):
Stewart, V.R. ( Rockwell International Corp. )  
Publication title:
NASA Technical Reports
Pub. Year:
1987
Issue:
NASA-CR-178348
No.:
G3/02 0097190
Pt.:
NAS1.26:178348
Paper no.:
N87-27641
Page(from):
1
Page(to):
96
Pages:
96
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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