Technical Report Archive & Image Library (TRAIL) - 136 Matching Results

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Preliminary Calculation of Cylinder Dimensions for Aircraft Engines

Description: It is extremely important in building aircraft engines to determine the requisite cylinder dimensions as accurately as possible, in order that the weight required for a given power shall not be excessive. This report presents a calculation method that depends on the air requirement of the fuel.
Date: September 1921
Creator: Schwager, Otto
Partner: UNT Libraries Government Documents Department
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Glossary of Terms Used in Flying Boat Hull Construction

Description: Memorandum presenting a glossary of terms used to describe flying boat hulls and the elements used in construction.
Date: September 1921
Creator: Nicolson, David
Partner: UNT Libraries Government Documents Department
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Competition for Safety Fuel Tanks

Description: Report describing a competition for safety fuel tanks, including the prizes, requirements that must be fulfilled, some other characteristics, tests, and regulations.
Date: September 1921
Partner: UNT Libraries Government Documents Department
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The Small Diesel Engine as an Automotive Engine

Description: Essential principles for building small diesel engines and also structural details so far as feasibility are presented.
Date: September 1921
Creator: Frey, Ernst
Partner: UNT Libraries Government Documents Department
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A New Dynamometer Brake

Description: The mechanism here described belongs to the class of dynamometer brake in which the motive power is transformed into heat in the brake itself. This mechanism was invented by the writer for the purpose of measuring forces in which the two factors, torque and speed, vary within broad limits, the mechanism itself being of simple construction and of still simpler operation.
Date: September 1921
Creator: Segrè, Marco
Partner: UNT Libraries Government Documents Department
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The 1000 HP Traffic Airplane of the Zeppelin Works in Staaken

Description: Report details the characteristics and advantages of the swift traffic airplane constructed by Zeppelin Works at Staaken. The maximum speed, weight, construction, layout, and landing capabilities of the plane are included.
Date: September 1921
Creator: Rohrbach, A. K.
Partner: UNT Libraries Government Documents Department
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Aerodynamic Laboratory at Cuatro Vientos

Description: This report presents a listing of the many experiments in aerodynamics taking place at Cuatro Vientos. Some of the studies include: testing spheres, in order to determine coefficients; mechanical and chemical tests of materials; and various tests of propeller strength and flexibility.
Date: September 1922
Creator: Jubera
Partner: UNT Libraries Government Documents Department
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Fatigue Resistance of Duralumin

Description: Where, in the following report, mention is made of fatigue, it always refers to the weakening of the material produced by rapidly changing stresses below the point of elasticity. The alternating stress was obtained by a test bar which was held at one end and subjected to rotation. Most of the tests were conducted on connecting rods.
Date: September 1922
Partner: UNT Libraries Government Documents Department
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Problem of Glider Models

Description: Any one endeavoring to solve the problem of soaring flight is confronted not only by structural difficulties, but also by the often far more difficult aerodynamic problem of flight properties and efficiency, which can only be determined by experimenting with the finished glider. The report primarily considers open-air experiments with glider models and some specific elements of gliders that have been studied using these experiments.
Date: September 1922
Creator: Espenlaub, Lippisch
Partner: UNT Libraries Government Documents Department
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Wind Vane With Various Applications

Description: A design for a wind vane is presented and various applications are discussed. The equations that can be used to calculate effects on the aircraft using the vane and control assistance that can be provided using the wind vane are provided.
Date: September 1922
Creator: Constantin, M. Louis
Partner: UNT Libraries Government Documents Department
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Giant Airplanes

Description: It is hardly possible for the most imaginative aeronautical enthusiast to look forward to a time when the airplane will have reached the dimensions commensurate with those already attained by the airship.
Date: September 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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International Aspects of Air Travel

Description: This article discusses two areas of international air travel, namely, passports and customs, as well as smuggling.
Date: September 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Aerodynamic Computation of Gliders

Description: From Introduction: "In the following discussion, a knowledge of the theoretical principles of airplane construction is assumed, as presented in detail by Vogt and Lippisch in Nos. 7 and 10-19 of the 1919 volume of this publication. A few quantities will however be otherwise designated, in accordance with the Gottingen symbols."
Date: September 1922
Creator: Schrenk, M.
Partner: UNT Libraries Government Documents Department
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Miniature Airplanes

Description: The present report will treat only the smallest airplanes equipped with engines. The two types discussed are those airplanes with the smallest dimensions, and those that have the smallest power requirements.
Date: September 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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The Disposal of Military Aircraft

Description: "The end of the war saw every belligerent with vast stocks of aircraft and aircraft supplies in all stages of usefulness, much of the material being absolutely new. The question of the best method of getting rid of this accumulation is one which has been agitating those responsible for its disposal for more than three years now, but no wholly satisfactory solution has yet been reached" (p. 1).
Date: September 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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What Retards Air Transport?

Description: The decrease in air traffic on the London-Paris route is examined and possible solutions are presented.
Date: September 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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The Prevention of Fire in the Air

Description: On an airplane, the safeguards adopted may be divided into three classes, those intended to prevent a fire from getting started, those intended to put it out if it does get under way, and, finally, those designed to limit the damage which a fire can do. Some of the fire-related elements discussed include protecting the gasoline, fire extinguishers, a flame-tight bulkhead, and airship hazards.
Date: September 1922
Creator: Warner, Edward P.
Partner: UNT Libraries Government Documents Department
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Provisional Rules for the Inspection of Aircraft Adopted by the French Bureau Veritas

Description: These new regulations are intended to replace those of November 1, 1922, and give the directions to be followed in the supervision of aircraft by the agents of the Aeronautical Section of the Bureau Veritas. The rules consist of four sections: rules regarding an aircraft leaving a repair shop, the objects of quarterly and weekly inspections, and rules regarding the upkeep and repair of airplanes.
Date: September 1924
Partner: UNT Libraries Government Documents Department
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Effect of Ratio Between Volume and Surface Area of Airships

Description: Report presenting an exploration of the concept that the ratio between the volume and the surface area also exerts an influence on other secondary characteristics of airships.
Date: September 1924
Creator: Crocco, G. A.
Partner: UNT Libraries Government Documents Department
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Recent Researches in Airship Construction 3: A New Type of Nonrigid Airship

Description: The author describes experiments in designing nonrigid airships. A nonrigid airship of 32,000 cubic meters, the PL 27 withstood all stresses with 20 kg/m(exp 2) hull pressure during its life of two years. The moment of resistance is known, as also the stresses in the envelope for the given hull pressure. The mean internal pressure necessary to give the airship the requisite rigidity and to prevent buckling was also investigated.
Date: September 1924
Creator: Naatz, H.
Partner: UNT Libraries Government Documents Department
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General Rules for Metal Aircraft Construction

Description: "The Commissariat of Aviation deems it expedient to issue a few rules of a general character which should be followed by constructors in designing aircraft, into the manufacture of which metal enters to a considerable extent. The materials covered include: aluminum, duralumin, soft steel, high-resistance steel, in sheets, tubing, and shaped elements" (p. 1).
Date: September 1924
Creator: Guidoni, Alessandre
Partner: UNT Libraries Government Documents Department
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The Effect of Free-Stream Turbulence on Heat Transfer From a Flat Plate

Description: Turbulence was generated by using screens, and the turbulence percentage was measured by a hot-wire anemometer both in the boundary layer and the free stream. The local heat-transfer coefficient was measured at 12 locations along the plate for the cases of various turbulence levels. The transition Reynolds number from laminar to turbulent flow decreases as the main-stream turbulence level increases. In the range of laminar heat transfer the effect of turbulence in the main flow was not great, b… more
Date: September 1958
Creator: Sugawara, Sugao; Sato, Takashi; Komatsu, Hiroyasu & Osaka, Hiroichi
Partner: UNT Libraries Government Documents Department
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Optimum Flight Paths of Turbojet Aircraft

Description: "The climb of turbojet aircraft is analyzed and discussed including the accelerations. Three particular flight performances are examined: minimum time of climb, climb with minimum fuel consumption, and steepest climb. The theoretical results obtained from a previous study are put in a form that is suitable for application on the following simplifying assumptions: the Mach number is considered an independent variable instead of the velocity; the variations of the airplane mass due to fuel consum… more
Date: September 1955
Creator: Miele, Angelo
Partner: UNT Libraries Government Documents Department
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Finite Span Wings in Compressible Flow

Description: Equations are developed using the source distribution method for the velocity potential function and pressure on thin wings in steady and unsteady motion. Closed form solutions are given for harmonically oscillating wings of general plan form including the effect of the wing wake. Some useful examples are presented in an appendix for arrow, semielliptical, and hexagonal plan form wings.
Date: September 1956
Creator: Krasilschchikova, E. A.
Partner: UNT Libraries Government Documents Department
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