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Calculation of Tapered Monoplane Wings
The tapered wing shape increases the lift in the middle of the wing and thus reduces the bending moment of the lifting forces in the plane of symmetry. Since this portion of the wing is the thickest, the stresses of the wing material are reduced and desirable space is provided for stowing the loads in the wing. This statically excellent form of construction, however, has aerodynamic disadvantages which must be carefully weighed, if failures are to be avoided. This treatise is devoted to the consideration of these problems.
Date:
August 1930
Creator:
Amstutz, E.
System:
The UNT Digital Library
Theory of the Landing Impact of Seaplanes
The present investigation is an endeavor to express the jolting stresses, designated as landing impacts, undergone by seaplanes in landing and taking off from rough water, as functions of specific factors, in order to enable the evaluation of empirically obtained results and thus acquire theoretical data for the construction of seaplane floats and hulls.
Date:
August 1930
Creator:
Pabst, Wilhelm
System:
The UNT Digital Library
Structural Details of German Light Airplanes
This report presents a review of German light airplane construction. Some of the topics discussed include: engines, fuselages, wings, landing gear, and other mechanical parts.
Date:
August 1930
Creator:
Schrenk, Martin
System:
The UNT Digital Library
Determination of the Best Cross Section for a Box Beam Subjected to Bending Stresses
Previous investigations on the strength characteristics and structure of wood in construction are analyzed and a method of representation is developed suitable for the use of designers.
Date:
August 1930
Creator:
Von Baranoff, A.
System:
The UNT Digital Library