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NASA Memorandum [NASA MEMO 4-20-59A]: Static stability and control of canard configurations at mach numbers from 0.70 to 2.22- lateral-directional characteristics of an unswept wing and canard

By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Peterson, Victor L.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Memorandum. Publisher: Nasa, Washington, D.C. 1959Description: 32p.Subject(s): Canard airplane configurations | Canard airplane --Sstatic stability and control
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Bound together NASA MEMO 4-14-59A to 4-27-59A
Lack No.4-16 to 4-17, 4-22 to 4-25

Bound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615

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