Technical Report Archive & Image Library (TRAIL) - 1,438 Matching Results

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Proposed Air Traffic Law

Description: This report presents a brief history of France's attempts to promulgate an internal air traffic law and then provides a draft of proposed national air traffic laws.
Date: May 1922
Creator: Ripert, Georges
Partner: UNT Libraries Government Documents Department
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Regulation of Air Traffic

Description: The ways in which the international and internal French air traffic accords interact with each other is outlined in this report. The principal questions covered by the present legislation are as follows: 1) Conditions of safety which must be fulfilled by aircraft; 2) Licenses for members of the crew; 3) Traffic rules to be observed by French and foreign aircraft.
Date: May 1922
Creator: Devaluez
Partner: UNT Libraries Government Documents Department
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Stability of Airplanes

Description: The author attempts to correct the misconception that piloting an airplane requires extraordinary skill and balance. He also tries to show that airplanes are extremely stable in flight. Some of the major points covered in this article include: automatic pilots, airplanes designed to be stable, and the reliance on mathematics to help in designing stable aircraft.
Date: May 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Subsidies for Air Transport

Description: This article discusses the need for government subsidies to encourage the development of passenger and freight transport by air.
Date: 1922-05?
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Technical Problems of Commercial Flying

Description: The technical requirements for commercial aircraft are listed, which include: safety, economy and comfort. The author lists various methods to increase these requirements in commercial aircraft.
Date: May 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Comfort in Flight

Description: Some advances in passenger comfort are discussed, namely, ventilated cabins, heating, seating arrangements, and doors.
Date: June 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Effect of Structure in Middle Part of Leading Edge of a Thick Wing: Communication From Rijks-Studiedienst Voor De Luchtvaart of Amsterdam

Description: The experiments herein described were made for the purpose of finding whether removing a larger portion of the wing to improve the pilot's view would be possible, without too great detriment to the aerodynamic properties of the airplane. The experiments were conducted on a wing similar to the Fokker F III.
Date: June 1922
Partner: UNT Libraries Government Documents Department
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Engine Pistons of Light Metal

Description: This report presents the results of testing 32 sets of light metal pistons from 16 different aluminum and magnesium alloys, 2 sets of cast iron pistons, and one piston of pure electrolytic copper. The many-fold mutual relations between material properties, shape, thermic and dynamic processes in the engine were clarified by comprehensive technical, thermic, chemical, physical and metallographic investigations of pistons and piston materials.
Date: June 1922
Creator: Becker, G.
Partner: UNT Libraries Government Documents Department
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Fakir Fuel Pump

Description: "In designing the Fakir fuel pump, the fundamental idea was to obtain a simple and reliable method of conveying the fuel from a low tank to the carburetor, with the avoidance of the faults of all former methods and the simultaneous warming of the fuel by means of the heat of compression generated. The principle of the Fakir fuel pump rests on the well-known principle of the diaphragm pump, which must be suitably adapted to the present purpose" (p. 1).
Date: June 1922
Partner: UNT Libraries Government Documents Department
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Problem of the Slotted Wing: A Communication From the Aerodynamic Institute of the Aachen Technical High School

Description: "It is to be expected that the advantageous properties, hitherto discovered in many slotted wing sections, depend very largely on the contour of the slot and the structural details of the wing. It is therefore of interest, aside from measurements on wings of constant cross-section along the span, to measure also wing models in which the structural details have already been given practical consideration" (p. 1).
Date: June 1922
Creator: Klemperer, W.
Partner: UNT Libraries Government Documents Department
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The Prospects of the Helicopter

Description: The advantages of helicopters are listed along with a discussion of safety devices, the problems of control, and the need for horizontal flight.
Date: June 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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The R-38 Catastrophe and the Mechanics of Rigid Airship Construction

Description: An airship frame may be regarded as a rigid girder subjected to a number of forces which, according to their nature, may be classified as follows: weight or loads (force of gravity); lifting forces (aero-static); accelerations (dynamic). These forces must be in equilibrium in the three most important cases during flight: 1) when the airship is floating (aerostatic problem); 2) when flying without acceleration (aerodynamic problem). 3) When under the influence of any accelerating force (dynamic … more
Date: June 1922
Creator: Herrera, Emilio
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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Aerial navigation by dead reckoning

Description: Report discussing the problem to be solved, as presented to the pilot or observer of an aircraft, is as follows: The aircraft starting from A must land at B, the only data being the speed of the airplane, the altitude and the orientation D of the course. The above data would be amply sufficient, were it not for the fact that the airplane is constantly subjected to a wind of variable direction and strength.
Date: July 1922
Creator: Maffert, Pierre
Partner: UNT Libraries Government Documents Department
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Aerodynamics and Ballistics

Description: Ballistics is a science hundreds of years old and this report is an attempt to show how these older principles can be used in the newer science of aerodynamics.
Date: July 1922
Creator: Burzio, Filippo
Partner: UNT Libraries Government Documents Department
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Airplane Stability Calculations and Their Verification by Flight Tests

Description: For some time, the designers of airplanes have begun to occupy themselves with the question of longitudinal stability. In their quest to simplify calculation and data collection, the designers have attached the greatest importance to the coefficient of initial longitudinal stability. In this study a diagram was constructed from the data of the tunnel tests, which depends neither on the position of the center of gravity nor of the angle of deflection of the elevators. This diagram is constructed… more
Date: July 1922
Creator: Rota, Augusto
Partner: UNT Libraries Government Documents Department
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Aviation in the Belgian Congo

Description: The establishment of air service in the Belgian Congo is detailed in this report. The airplanes, landing fields, and air routes are all discussed.
Date: July 1922
Creator: van Crombrugge, A.
Partner: UNT Libraries Government Documents Department
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European Air Travel in 1922

Description: This article discusses the different passenger air transport services offered in Europe. The author deals mainly with the service offered between different cities, in terms of time and cost.
Date: July 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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General Problem of the Airplane

Description: A series of equations relating to airplanes are given and examples listed. Some of the equations listed include: the speed, altitude and carrying capacity of various airplanes; weight of an airplane; weight of various parts of an airplane; the polars of the wings; speeds of airplanes; radius of action.
Date: July 1922
Creator: Richard, Maurice & Richard, Paul
Partner: UNT Libraries Government Documents Department
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Laying out of a practical air route

Description: Unfortunately the problem of laying out an air route has been approached by all who give it consideration as one of the hardest tasks in the world. Whereas, as a matter of fact, a very serviceable air route can be laid out with an absolute minimum of ground work.
Date: July 1922
Creator: Miner, V. S. & Carroll, T.
Partner: UNT Libraries Government Documents Department
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Maritime Aviation

Description: This report presents some studies of maritime aviation which cover the following principal points: employment of landplanes on maritime aerial warfare; their adaption to peculiar requirements of the Navy; and the establishment of a method of aerial pursuit and bombardment, likewise adapted to military aviation over land.
Date: July 1922
Creator: Ravennes, Jean
Partner: UNT Libraries Government Documents Department
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