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Rigid Airships

Description: Memorandum presenting the history and development of airships. Tables containing information and statistics regarding some of the current airships are provided.
Date: November 1923
Creator: Stahl, Friedrich
Partner: UNT Libraries Government Documents Department
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Monoplanes or Biplanes?

Description: This article presents a discussion of the relative merits between monoplanes and biplanes. A comparison of the aerodynamic qualities and advantages of both types are provided.
Date: November 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Factors of Safety

Description: Factors of safety serve three purposes: provides against trouble arising from unexpectedly large loads, allows for imperfections of workmanship, represents a depreciation allowance. A consideration of these safety factors is provided in this report.
Date: December 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Seaplanes for Commerce

Description: The advantages of using seaplanes for commercial purposes is discussed. The three primary advantages described include their superior speeds over existing means of transport on the same routes, the available landing fields when flying over the water, and the reduction of distance from the airport to the city is serves due to the seaplane's ability to land in water.
Date: March 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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My Experience With Helicopters

Description: The author recounts his experiments with helicopters. The object of his investigations was to remain stationary in the air for five minutes and to make a closed flight at low altitude. Some of the topics discussed include stabilization, horizontal flight, and directional control.
Date: April 1923
Creator: Oemichen, Etienne
Partner: UNT Libraries Government Documents Department
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Wind-Driven Propellers (Or "Windmills")

Description: Wind-driven propellers are much used as sources of power for equipment such as radios. This report establishes the principles involved and acquaints the reader with rules for design of such windmills.
Date: April 1923
Creator: Munk, Max M.
Partner: UNT Libraries Government Documents Department
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Wind Tunnel of Zeppelin Airship Company

Description: This report discusses the general considerations for the design of aerodynamic laboratories. The dimensions, construction, and components of the wind tunnel are given special attention.
Date: April 1923
Creator: Munk, Max M.
Partner: UNT Libraries Government Documents Department
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New Albatross Commercial Airplane "L 58"

Description: The "L 58" is a monoplane with cantilever wings joined directly to the fuselage. It accordingly belongs to the new school of airplane construction, as founded and developed in Germany. A list of performance characteristics is included.
Date: March 1923
Creator: Meyer, G.
Partner: UNT Libraries Government Documents Department
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The New Interpretation of the Laws of Air Resistance

Description: A closer examination of Newton's formula for air resistance shows that it is well to consider the air as an ordinary fluid, and, indeed for most of the velocities considered, as a non-compressible fluid, so long as the dimensions of the moving body are large in comparison with the mean free path of the particles of air.
Date: April 1923
Creator: Prandtl, L.
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 Controls of an Airplane

Description: The control of an airplane is discussed beginning with sideways motion and following up with control by weight shifting and by swinging wing tips.
Date: June 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
open access

Variable Pitch Propeller

Description: The advantages of variable pitch propellers over constant pitch propellers is presented along with different methods of varying the pitch. The technique of varying the shape of the propeller is presented as the most efficient one.
Date: July 1923
Creator: Pistolesi, Enrico
Partner: UNT Libraries Government Documents Department
open access

Control Operating Mechanisms for Airplanes

Description: The connections between the cockpit and the control surfaces are examined. An examination of the pros and cons of using stick control, the problems of control in giant aircraft, an effort to find a substitute for these controls, and a proposed concept for mechanically operated gear are provided.
Date: July 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
open access

The "Autogiro"

Description: Report presenting a description of the autogiro, which is a flying machine built and designed in Spain. A history of the device and the reasons why it is safer and more stable than a typical aircraft are provided.
Date: July 1923
Creator: Moreno-Caracciolo, M.
Partner: UNT Libraries Government Documents Department
open access

Control Problems on Large Airplanes

Description: The development of more efficient control surfaces requiring less force to operate are presented. Some of the control surfaces explored include the De Havilland gear, Flettner rudder, and some other possible control methods.
Date: July 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Possible Improvements in Gasoline Engines

Description: High-compression engines are investigated with the three main objects being elimination of vibration, increase of maximum efficiency, and conservation of this efficiency at the highest possible speeds.
Date: January 1923
Creator: Ziembinski, S.
Partner: UNT Libraries Government Documents Department
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Soaring Without Rising Currents

Description: Memorandum describing the main problem of soaring flight, which is that it is difficult to maintain altitude and to engage in indefinite continuation of flight without dependence on rising currents from any source. The best chance of success involves utilizing energy stored in the air when the wind speed is constantly and rapidly varying.
Date: February 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
open access

Lessons of the 1922 Rhön Soaring Flights

Description: Innovations in design and technique from the Rhön soaring contest are presented in this report.
Date: February 1923
Creator: Prandtl, L.
Partner: UNT Libraries Government Documents Department
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Bird Flight: Hints to Be Obtained From It for Use in Aviation

Description: This report is a comprehensive study of birds and how their shapes have been molded by the resistance of the air. 500 species of birds were studied and nearly 30,000 ratios calculated. The author makes a distinction between flapping and soaring flight.
Date: August 1923
Creator: Magnan
Partner: UNT Libraries Government Documents Department
open access

The Effect of Bow Stiffeners in Nonrigid Airships

Description: "It is now well known that all nonrigid airships constructed at the present time have bow stiffeners consisting of battens curved to the form of the envelope and designed to hold the nose of the ship in its true form despite the very large pressure which exists at the extreme forward point. The effect of the stiffeners is to reduce considerably the apparent pressure which has to be maintained inside the envelope in order to prevent the nose from caving in" (p. 1).
Date: August 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
open access

Airplane Speeds of the Future

Description: While the reliability of predictions is poor the author still attempts to gauge the future speeds of airplanes.
Date: January 1923
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Marcel Besson Wing Sections

Description: Three different Marcel Besson airfoils are investigated in terms of maximum lift, maximum fineness, minimum required power, and wing section drag. Comparisons are then made between the three airfoils.
Date: January 1923
Creator: Delanghe, C.
Partner: UNT Libraries Government Documents Department
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