Within limitations of linearized potential theory for supersonic flow, solutions have been obtained for damping in roll of triangular, trapezoidal, rectangular, and two sweptback plan forms.
Damping due to roll of triangular, trapezoidal, and related plan forms in supersonic flow
Nat Advisory Committee Aeronautics -- Tech Note
1948
18 pages
6 Supp sheets
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1948
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