Geometric variables covered included horizontal-tail chord, horizontal tail-span, vertical location of horizontal tail, and horizontal-tail dihedral angle; calculations were restricted to configurations having vertical tail of aspect ratio 1.0.
Effect of horizontal-tail chord on calculated subsonic span loads and stability derivatives of isolated unswept tail assemblies in sideslip and steady roll
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 4-1-59L
1959
32 pages
Report
English
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Engineering Index Backfile | 1953
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