National Advisory Committee for Aeronautics (NACA) - 1,438 Matching Results

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The Wing With a Pointed Tip

Description: In airplane construction generally one finds an almost exclusive use of wing tips that are practically square end but occasionally those with large rounded tips. For use as a cantilever wing, however, a wing with pointed tips may contain valuable aerodynamic advantages.
Date: October 1922
Creator: v. Prondzynski, Stephan
Partner: UNT Libraries Government Documents Department
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Wings With Nozzle-Shaped Slots

Description: Even before the publication of the results of the Gottingen experiments on the removal of the boundary layer by suction, experiments with nozzle-slotted wings were begun. A report of those experiments will be given here. Taken collectively, the experiments show that, as regards increasing the lift values, the effect of the air flowing from the nozzle-shaped slots is similar to the effect produced in the case of ordinary slotted wings. The high lift values are attained, however, at the smaller a… more
Date: July 1929
Creator: Katzmayr, Richard
Partner: UNT Libraries Government Documents Department
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Wire Suspensions in Wind Tunnel Experiments

Description: The elimination of the rigid supports for models and their replacement by wires constitute a great improvement by rendering negligible the interactions of support. There are disadvantages to wire, namely, the aerodynamic resistance is very large and their use is rather difficult because the whole suspension lacks rigidity and easily becomes distorted. We will here investigate the nature of these distortions, evaluate the errors they entail and describe the methods for taking account of or avoid… more
Date: December 1925
Creator: Kerneis, Jean
Partner: UNT Libraries Government Documents Department
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Wood Versus Metal in Airplane Construction

Description: The aim of this article is to present, in broad outline, a scientific method for solving the problem, "Wood or Metal." It will be shown that structural methods have by no means reached their final perfection. The strength of the different materials is discussed as well as different construction methods.
Date: June 1923
Creator: Seehase, H.
Partner: UNT Libraries Government Documents Department
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Wood Versus Metal in Airplane Construction

Description: The aim of this article is to present, in broad outline, a scientific method for solving the problem, "Wood or Metal." It will be shown that structural methods have by no means reached their final perfection. The strength of the different materials is discussed as well as different construction methods.
Date: June 1923
Creator: Seehase, H.
Partner: UNT Libraries Government Documents Department
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The World's Air Transportation Services: Data as to Passengers, Mail, and Goods Carried by American and European Transportation Services

Description: This report presents detailed descriptions, statistics, and graphs on European and American air transport. The European countries listed are Belgium, Czecho-Slovakia, Denmark, France, Germany, Great Britain, Holland, and Italy.
Date: June 1922
Creator: Office of Aeronautical Intelligence
Partner: UNT Libraries Government Documents Department
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Wrinkling of Reinforced Plates Subjected to Shear Stresses

Description: An analysis is made here of the problem of long plates with transverse stiffeners subject to shear. A typical example would be a long Wagner beam. The shear stress is calculated at which the web wrinkles and shear stress becomes a maximum. The equation is solved for both a condition of free support and rigidity of support on the edges.
Date: January 1931
Creator: Seydel, Edgar
Partner: UNT Libraries Government Documents Department
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Wrinkling Phenomena of Thin Flat Plates Subjected to Shear Stresses

Description: This report covers a series of tests on thin flat elastic strips restrained at two parallel edges and subjected to shear by conversely directed stresses. Theoretical treatments, particularly those of Lilly, Southwell and Skan, and Timoshenko are briefly outlined. The problem to be solved by these tests was to find out whether, and to what extent the conditions and assumptions upon which the calculations are based are complied with in the tests.
Date: January 1931
Creator: Bollenrath, F.
Partner: UNT Libraries Government Documents Department
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