Study of supersonic wings employing the attainable leading-edge thrust concept

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National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982 - Technology & Engineering - 159 pages
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Contents

Effect of Increased LeadingEdge Radius Wing 3Flat
1
Planform Characteristics Wing 8 47
8
Relationship Between Streamwise and Normal Wing Sections
11

20 other sections not shown