Москва: Авиация, — 324 с. Институтский курс "Расчет самолета на прочность". Содержит основные методики расчета деталей узлов и агрегатов ЛА. Курс предназначен студентам и полезен для инженеров, занимающихся проектировочным расчетом самолетных агрегатов и конструкций.
Издание 4-е, переработанное. — М.: Госиздат Оборонной промышленности, 1958. — 292 с. Книга является учебником по расчёту самолета на прочность, переработанным и дополненным авторами по сравнению с изданием 1945 г. В учебнике изложены вопросы: определения нагрузок, действующих на самолет, рассмотрены методы расчета крыла, оперения, фюзеляжа, установок под двигатели, узловых...
Диссертация на соискание ученой степени кандидата технических наук. Специальность 01.02.06 Динамика, прочность машин, приборов и аппаратуры. — М.: Институт машиноведения, 2016. — 213 с. Одним из основных условий развития современной промышленности и повышения уровня обороноспособности страны является применение новых конструкционных материалов, позволяющих улучшить технические...
Moscow: Mashinostroyeniye, 1971. — 312 p. This book presents diagrams of helicopters, design, kinematic and power diagrams of the basic components of domestic series-produced helicopters, general data on the process of designing a helicopter and necessary information from the history of helicopter construction development. The weight perfection of a helicopter, its reliability 4...
London, New York: McGraw-Hill Book Company, 1930. — 294 p. A propeller is a device for providing a force or thrust, at the expense of power generated by a motor, for driving a craft of some type through a fluid medium, such as air or water. In order to provide this thrust, the propeller must set a mass of the fluid in motion in a direction opposite to that of the craft being...
Connecticut: United Aircraft Corporation, 1971. — 206 p. Prepared under Contract No. NAS2-5885. Aviation forecasts for the ne_ ten to fifteen year time period, indicate continued steady growth of general aviation. The attainment of this forecasted growth and even a more rapid expansion is dependent upon the continued improvement in the safety, utility, performance and cost of...
Диафильм. — Казань: Казанский Институт повышения квалификации кадров Министерства Авиационной промышленности, 1986. — 97 с. Художники: Буташнов В.Т., Камалов И.Ш., Аглиуллова Н.А. К программе подготовки и повышения квалификации сборщиков - клепальщиков.
Bloomfield: Caman Aerospace Corp., 1976. — 165 p. This report examines the design of major helicopter components and its effect on the man-hour cost of field repair. Recommendations are developed for improving the field repairability of these components on future helicopters through improved applications of current technology and new design concepts. The study was accomplished...
Submitted in partial fulfillment of the requirements for the degree of Master of Science in Aeronautical Engineering. — Monterey: Naval Postgraduate Schoo, 1983. — 122 p. A conceptual helicopter design method utilizing closed form formulas and approximations from historical data is developed for use in a helicopter design course. The design manual is to be used for the...
Third printing. — London: Chapman & Hall Ltd, 1948. — 128 p. The aircraft propeller consists of two or more blades and a central hub to which the blades are attached. Each blade of an aircraft propeller is essentially a rotating wing. As a result of their construction, the propeller blades are like airfoils and produce forces that create the thrust to pull, or push, the aircraft...
Author not specified. — Alexandria: Army Materiel Command, 1974. — 880 p. This handbook discusses the design requirements applicable to Army helicopters for all missions under visual flight rule (VFR) operation, day or night. As such, the scope of this document has been limited to cover the basic aerial vehicles. Design requirements for mission-essential equipment-e.g., weapons,...
Langley: Langley Research Center, 1980. — P. 405 - 420 General Aviation Aircraft represent a cost effective solution to many of the public's transportation problems. Due to their fuel efficiency, propeller driven commuter aircraft are appearing in ever increasing numbers, replacing jet CTOL's on short block time, low passenger density routes. Business aircraft have experienced a...
Translate into Russian. — Washington: National Aeronautics and Space Administration, 1968. — 470 p. There are 35 tables, illustrations, and 47 references. Translation of "Vertolety. Raschet i proyekt irovaniye. Том 2. Kolebaniya i dinamicheskaya prochnost." — Moscow: “Mashinostroyeniye” Press, 1967. The second volume gives an account of certain problems of the theory of...
Snyder Samuel F., Voorhees Gene C., Heinrich Allyn M., Baisden Donald N. — Wichita: NASA, 1977. — 166 p. During this study, the conceptual design of a four place single turbofan ' engine powereo light airc-raft was accomplished utilizing contemporary light aircraft conventional design techniques as a means of evaluating the NASA-Ames General Aviation Synthesis Program (GASP) as...
Washington: Langley Memorial Aeronautical Laboratory, 1935. — 18 p. A method has been devised for determining the frequencies of the various modes of a stationary propeller and the associated crankshaft. A method has also been devised to obtain the effect of the centrifugal force on a revolving propeller by use of a flexible model.
Revised Edition, Second Printing. — New York: Roland Press Company, 1944. — 146 p. The information is presented in the same style, understandable rather than extremely technical, which contributed to the success of the first edition. All equations are given in the most simplified forms, employing advanced mathematics only where it could not be avoided. The aim has been to meet...
New York: D. Van Nostrand Company, 1912. — 78 p. The Aeroplane Air Pressure Weight and Power Propellers and Motors Balancing Construction Difficulties Future Developments Other Flying Machines (Gyroplane and Ornithoptere)
Fifth Edition, Seventh Impression. — New York: McGraw-Hill Book Company Inc, 1942. — 784 p. The building and maintenance of the modem airplane require a knowledge of many things. The most vital need is absolute reliability on the part of designers, the mechanics, the maintenance men or ground crew, and the pilot. Aside from the needed skill is the need for dependability in all...
Blue Bell: Dynasciences Corporation, 1967. — 190 p. A theoretical and experimental study was conducted to determine the effects of propeller slipstream on wing performance. Previously developed theoretical analyses were expanded and modified to account for radial variation of the propeller slipstream velocity. The experimental program consisted of wind tunnel tests conducted...
Melbourne: Department of Defence Support Defence Science and Technology Organisation Aeronautical Research Laboratories, 1982. — 26 p. In this Note a model of the dvnamic motion of a single-engine propeller-driven aircraft has been used to illustrate a longitudinal stabilit" problem caused br the effects of power. In a recent general study on the effects of power the problem wvas...
National Aeronautics and Space Administration Levis center, 1980. — P.315-325 A program on propeller technology applicable to both low and high speed general aviation aircraft is summarized, and the overall program objectives and approach are outlined.
New York: D. Van Nostrand Company, 1910. — 146 p. Only yesterday aviation was born ; to-day it has already called into being a vast representative industry whose future is definitely assured. Two years have passed since that great day when we stood on the manoeuvring ground of Issy-les-Moulineaux, waiting anxiously to see the Voisin aeroplane, piloted by Farman, rise and fly....
Thesis. — Cranfield: The College of Aeronautics, 1962. — 66 p. This thesis analyzes the first order effects of aerodynamic design parameters for convertiplane propeller-rotors when operating in hovering and cruising flight, and a criterion for obtaining optimum combinations of these parameters is established
Староверов Н.Е. F02K 7/16, F02K 7/18. Заявка: 18.09.2012. — 6 с. В гиперзвуковом двигателе, содержащем камеру сгорания, топливо после топливного насоса и перед подачей в камеру сгорания нагревается выше температуры самовоспламенения. Нагрев топлива происходит в теплообменнике, находящемся в стенках камеры сгорания или непосредственно в камере сгорания. Гиперзвуковой двигатель...
Author not specified. — Alexandria: Army Materiel Command, 1976. — 572 p. This volume Delail Design is Part Two of a three-part Engineering Design Handbook titled Helicopter Engineering Along with AMCP 706-201. Preliminary Design. and AMCP 706-203, Qualification A.tsurance, this part is intended to set forth explicit design standards for Army helicopters, to establish...
Kansas: University of Kansas - Department of Aerospace Engineering, 1988. — 40 p. Partially supported by NASA Langley Research Center. This special project was performed to study the basic aerodynamic characteristics of an ultra-light wing. Few known wind tunnel tests have been performed of ultra-light wings since they are designed to be very inexpensive. Thus, aerodynamic data...