No. 325: Data on actual aerodynamic forces and resulting stresses and bending moments in hull of U.S.S. Los Angeles, during severe still-air maneuvers, and in straight flight during rough air; maximum stresses within limits provided in accepted practice; flight in rough air produced forces and stresses about twice as great as most severe still-air maneuvers; transverse aerodynamic forces on hull proper small and irregular; coefficients of tail-surface forces and hull bending moments.
Speed and deceleration trials of U.S.S. Los Angeles
Nat. Advisory Committee Aeronautics -- Reports
1929
16 pages
16 Figs.
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Speed and deceleration trials of U.S.S. Los Angeles
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