Serial/Series Title

Drag Measurements on a Junkers Wing Section: Application of the Betz Method to the Results of Comparative Tests Made on a Model and on an Airplane in Flight (open access)

Drag Measurements on a Junkers Wing Section: Application of the Betz Method to the Results of Comparative Tests Made on a Model and on an Airplane in Flight

The comparison of model tests in flight can be based on the result of such measurements. They are very important from the aerodynamical point of view, as they lead to useful conclusions regarding the behavior of the wing, its best shape and the conformity of theoretical and actual flow. Although there still remains a certain prejudice against such measurements, I have still attempted to make these comparative tests in order to inspire confidence in their reliability.
Date: September 1927
Creator: Weidinger, Hanns
System: The UNT Digital Library
Building a Full-Size Glider (open access)

Building a Full-Size Glider

The building and flying of a glider is possible for anyone who can use a few basic tools. This report presents some plans and techniques for building your own glider.
Date: September 1927
Creator: Camm, F. J.
System: The UNT Digital Library
Effects of Roughness on Airfoils (open access)

Effects of Roughness on Airfoils

We will here report on the effects of coarsely roughening not only the pressure side but also the suction or upper side of airfoils, as the first group of a larger series of experiments.
Date: September 1927
Creator: Schrenk, O.
System: The UNT Digital Library
Experiments on airfoils with trailing edge cut away (open access)

Experiments on airfoils with trailing edge cut away

"Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of flying boats and the central section of the wings for affording better visibility. It was therefore of some interest to discover the effect of such cutaways on the lift and drag and on the position of the center of pressure. For this purpose, systematic experiments were performed on two different airfoils, a symmetrical airfoil and an airfoil of medium thickness, with successive shortenings of their chords" (p. 1).
Date: September 1927
Creator: Ackeret, J.
System: The UNT Digital Library
Seaplanes floats and hulls. Part 2 (open access)

Seaplanes floats and hulls. Part 2

Different float designs are presented and the investigations are discussed.
Date: September 1927
Creator: Herrmann, H.
System: The UNT Digital Library