Книги з теми "Torsion model"
Оформте джерело за APA, MLA, Chicago, Harvard та іншими стилями
Ознайомтеся з топ-18 книг для дослідження на тему "Torsion model".
Біля кожної праці в переліку літератури доступна кнопка «Додати до бібліографії». Скористайтеся нею – і ми автоматично оформимо бібліографічне посилання на обрану працю в потрібному вам стилі цитування: APA, MLA, «Гарвард», «Чикаго», «Ванкувер» тощо.
Також ви можете завантажити повний текст наукової публікації у форматі «.pdf» та прочитати онлайн анотацію до роботи, якщо відповідні параметри наявні в метаданих.
Переглядайте книги для різних дисциплін та оформлюйте правильно вашу бібліографію.
Takahashi, Marc D. A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. Moffett Field, Calif: NASA Ames Research Center, 1990.
James P. Smith - undifferentiated. Highly accurate beam torsion solutions using the p-version finite element method. [Washington, D.C.?: National Aeronautics and Space Administration, 1996.
Sedarat, Hassan. Torsional response characteristics of regular buildings under different seismic excitation levels. Sacramento: California Dept. of Conservation, Division of Mines and Geology, Office of Strong Motion Studies, 1994.
Atarod, Vida. Impact of synchronous machine constants and models on the analysis of torsional dynamics. Ottawa: National Library of Canada, 1992.
Hudson, James W. Development and calibration of a torsional engine model for a three-cylinder, two-stroke diesel engine. Monterey, Calif: Naval Postgraduate School, 1997.
Swanson, William J. Determination of diesel engine cylinder gas torques from speed fluctuations with a high-fidelity crankshaft torsional model. Monterey, Calif: Naval Postgraduate School, 1998.
A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. Moffett Field, Calif: NASA Ames Research Center, 1990.
A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. Moffett Field, Calif: NASA Ames Research Center, 1990.
Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. Moffett Field, Calif: NASA Ames Research Center, 1990.
Center, Langley Research, ed. Coupled bending-torsion steady-state response of pretwisted, nonuniform rotating beams using a transfer-matrix method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Coupled bending-torsion steady-state response of pretwisted, nonuniform rotating beams using a transfer-matrix method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Center, Langley Research, ed. Coupled bending-torsion steady-state response of pretwisted, nonuniform rotating beams using a transfer-matrix method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Sanford, Fleeter, and Lewis Research Center, eds. The predicted effect of aerodynamic detuning of coupled bending-torsion unstalled supersonic flutter. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Development and Calibration of a Torsional Engine Model for a Three- Cylinder, Two-Stroke Diesel Engine. Storming Media, 1997.
Determination of Diesel Engine Cylinder Gas Torques from Speed Fluctuations with A High-Fidelity Crankshaft Torsional Model. Storming Media, 1998.
Malen, Donald E. Fundamentals of Automobile Body Structure Design. 2nd ed. SAE International, 2020. http://dx.doi.org/10.4271/9781468601756.
Galderisi, Maurizio, and Sergio Mondillo. Assessment of diastolic function. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199599639.003.0009.
Lange, Joachim, and Henrik Uterwedde, eds. Frankreich und Deutschland. Nomos Verlagsgesellschaft mbH & Co. KG, 2019. http://dx.doi.org/10.5771/9783748904885.