Thematische Bibliographien / Airplanes

Auswahl der wissenschaftlichen Literatur zum Thema „Airplanes“

Autor: Grafiati
Veröffentlicht am 4. Juni 2021
Zuletzt aktualisiert am 30. Juli 2024

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Zeitschriftenartikel zum Thema "Airplanes"

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Kuzmin, Yu V. „Passenger airplane manufacturing in the 20th century. Quantitative analysis“. Civil Aviation High Technologies 26, Nr. 3 (23.06.2023): 8–24. http://dx.doi.org/10.26467/2079-0619-2023-26-3-8-24.

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The statistics on the production and development of passenger airplanes in the world is presented in this article for the first time. The methods for obtaining the results are described, uncertainties of the results are estimated. It is specified what exactly is considered to be a passenger airplane. It is shown that only 60,000 passenger airplanes were built during the entire 20th century. This is less than 3% of the total production of airplanes of all classes. Their total capacity amounts less than 5 million people, or less than a thousandth of the world’s population by the end of the last century. These 60,000 airplanes provided unprecedented mobility of the population. It was revealed that the leading role in the passenger airplane manufacturing belonged to the USA, the USSR took a steady second place. The ups-and-downs in airplane production are described, including the recessions during the Great Depression, World War II and the global economic decline (in the USSR, the USA and other countries) in the early 1960s, which was replaced by a rapid increase in output. It is indicated that the number of airplanes produced in the last third of the 20th century remained approximately constant, but their average capacity was growing rapidly, which largely ensured the explosive growth of air transportation during this period. The dynamics of the dead weight per one passenger is given. The dynamics of the number of the new passenger airplane models is presented. It is shown that for the last 30 years of the century their number was approximately constant, and almost all the models that reached the test stage were put into serial production. In the period between the world wars, however, about half of all models tested in flight remained prototypes. The change in the ratio of the number of airplanes by the number of engines is given. The renaissance of three-engine airplanes in the 1960s, the almost complete disappearance of singleengine passenger airplanes by the end of the century and the stable amount of a small proportion of four-engine airplanes for the last 30 years of the past century are noted.
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Rogalski, Tomasz, und Boguslaw Dołęga. „ALGORITHMS IMPROVING FLYING QUALITIES OF GENERAL AVIATION AIRCRAFT“. Aviation 10, Nr. 2 (30.06.2006): 17–21. http://dx.doi.org/10.3846/16487788.2006.9635930.

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The dynamic growth of general aviation as a mean of transport over medium distances means that people having no extraordinary qualifications or extraordinary physical or mental abilities more often pilot such types of airplanes. This phenomenon creates the necessity of giving planes flying qualities that allow them to be safely piloted by ordinary people. One way of solving this problem is equipping airplanes with fly‐by‐wire control systems that modify their handling qualities. Then the computer included into such control systems modifies the actions taken by the pilot, making the airplane both easier and more comfortable to control. This paper presents sample software tools – control algorithms that allowing an airplane's handling qualities to be improved. They are prepared by the authors and tested on board an experimental plane. That plane was equipped with a prototypical fly‐by‐wire control system, which can modify a plane's responses to a pilot's actions.
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Morad, Alaa M. „Multidisciplinary conceptual investigation for integrating stores, not in the original configuration of a subsonic airplane“. Journal of Physics: Conference Series 2616, Nr. 1 (01.11.2023): 012005. http://dx.doi.org/10.1088/1742-6596/2616/1/012005.

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Abstract Subsonic airplanes are widely used around the world in applications such as pilot training, transportation, sports activities, insect fighting, and field monitoring. This research deals with airplanes that already own the capability of carrying suspended loads. Increasing the airplane’s capabilities and configurations by integrating different suspended loads like smaller or larger external fuel tanks or insecticide tanks that are not in the original configuration of the airplane is a great advantage. This modification can be done without dramatic changes to the airplane and with minimum cost. In this research, a multidisciplinary methodology is used to integrate a commercially-available premade external fuel tank into the Embraer E312 Tucano airplane which is not in the original configuration of the airplane. First, a geometrical analysis is performed to ensure the availability of proper installation. This study leads to the design of an adaptor between the tank and the airplane pylon, then, a computational fluid dynamics (CFD) modeling using ANSYS-CFX is performed to evaluate aerodynamic forces and moments applied on the new fuel tank. Furthermore, finite element modeling using ANSYS-Static structure is performed by applying the aerodynamic and inertial loads to calculate the adaptor’s stresses and structure safety factor. Finally, vibration fatigue analysis-based power spectral densities are developed using ANSYS-Random vibration to calculate the adaptor’s estimated lifetime to ensure the store system’s safety by applying airplane vibration acceleration spectral density pattern selected from applicable standard. In this typical example, the above-mentioned methodology is applied and the results are acceptable.
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Shi, Fan, Fang Qiu, Xiao Li, Yunwei Tang, Ruofei Zhong und Cankun Yang. „A Method to Detect and Track Moving Airplanes from a Satellite Video“. Remote Sensing 12, Nr. 15 (25.07.2020): 2390. http://dx.doi.org/10.3390/rs12152390.

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In recent years, satellites capable of capturing videos have been developed and launched to provide high definition satellite videos that enable applications far beyond the capabilities of remotely sensed imagery. Moving object detection and moving object tracking are among the most essential and challenging tasks, but existing studies have mainly focused on vehicles. To accurately detect and then track more complex moving objects, specifically airplanes, we need to address the challenges posed by the new data. First, slow-moving airplanes may cause foreground aperture problem during detection. Second, various disturbances, especially parallax motion, may cause false detection. Third, airplanes may perform complex motions, which requires a rotation-invariant and scale-invariant tracking algorithm. To tackle these difficulties, we first develop an Improved Gaussian-based Background Subtractor (IPGBBS) algorithm for moving airplane detection. This algorithm adopts a novel strategy for background and foreground adaptation, which can effectively deal with the foreground aperture problem. Then, the detected moving airplanes are tracked by a Primary Scale Invariant Feature Transform (P-SIFT) keypoint matching algorithm. The P-SIFT keypoint of an airplane exhibits high distinctiveness and repeatability. More importantly, it provides a highly rotation-invariant and scale-invariant feature vector that can be used in the matching process to determine the new locations of the airplane in the frame sequence. The method was tested on a satellite video with eight moving airplanes. Compared with state-of-the-art algorithms, our IPGBBS algorithm achieved the best detection accuracy with the highest F1 score of 0.94 and also demonstrated its superiority on parallax motion suppression. The P-SIFT keypoint matching algorithm could successfully track seven out of the eight airplanes. Based on the tracking results, movement trajectories of the airplanes and their dynamic properties were also estimated.
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Endara Julio, Álvarez, Susan Sardinas Castellón, Parra Nigañes Patricia, Arancibia Marianela und Nuñes Prado Natalia. „Case report: Thrombosis in children“. Hematology & Transfusion International Journal 8, Nr. 5 (30.10.2020): 105–6. http://dx.doi.org/10.15406/htij.2020.08.00235.

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Objective: We examined the effects of passenger air transport by regular airplanes for air transportation on blood for transfusion. Materials and methods: Irradiated red blood cell (RBC) solutions were transported by regular passenger airplanes which and were static in the cabin during the flight. Blood samples were evaluated visually and biochemically before and after transport. Hemolysis of the transported samples was compared to that of the non-transported ones. The vibration in the airplanes was also measured using a vibration data logger. Results: There was no significant hemolysis of RBCs during airplane transport. The vibration in the airplane was lower than that in automobiles. The temperature in the active transport refrigerator (ATR) room was maintained at 2−6°C. There was no significant hemolysis of RBCs during the two transport routes. Conclusion: Temperature-controlled air transport of blood transport in the ATR 700 airplane maintained a the blood at a good quality that rendered blood it fit for blood transfusion.
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Yakushiji, Koki, Takanori Yokochi, Hiroshi Fujita und Fumiatsu Yakushiji. „Effects of passenger airplane transport on blood“. Hematology & Transfusion International Journal 8, Nr. 5 (30.10.2020): 108–9. http://dx.doi.org/10.15406/htij.2020.08.00236.

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Objective: We examined the effects of passenger air transport by regular airplanes for air transportation on blood for transfusion. Materials and methods: Irradiated red blood cell (RBC) solutions were transported by regular passenger airplanes which and were static in the cabin during the flight. Blood samples were evaluated visually and biochemically before and after transport. Hemolysis of the transported samples was compared to that of the non-transported ones. The vibration in the airplanes was also measured using a vibration data logger. Results: There was no significant hemolysis of RBCs during airplane transport. The vibration in the airplane was lower than that in automobiles. The temperature in the active transport refrigerator (ATR) room was maintained at 2−6°C. There was no significant hemolysis of RBCs during the two transport routes. Conclusion: Temperature-controlled air transport of blood transport in the ATR 700 airplane maintained a the blood at a good quality that rendered blood it fit for blood transfusion.
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Xiao, Boming. „Analysis on the relation between the vertex angle of a tube airplane and its flying time“. Theoretical and Natural Science 5, Nr. 1 (25.05.2023): 514–18. http://dx.doi.org/10.54254/2753-8818/5/20230310.

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The tube is a type of airplane that is shaped as a hollow cylinder. In common sense, it seems impossible that an airplane has no wings, however, the tube airplane can fly even longer in the sky comparing with normal airplanes. In this paper, the practical experiment related to Bernoullis theorem and Magnus Force will be introduced. In order to understand those equations more deeply with logic, a paper airplane model called the tube is going to be studied. The author makes the models with different shapes and angles so as to figure out the relationship between the angle of the index and the flying time of the airplane. Results show that the angle of the index has an impact on the time of the airplane staying in the sky, and the angle affects the angular and linear rotating speed of the airplane so that the time required for the airplanes varies.
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Kakinuma, Taro, und Masaki Hisada. „A Numerical Study on the Response of a Very Large Floating Airport to Airplane Movement“. Eng 4, Nr. 2 (21.04.2023): 1236–64. http://dx.doi.org/10.3390/eng4020073.

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Numerical simulations were generated to investigate the response of a floating airport to airplane movement using the nonlinear shallow water equations of velocity potential for water waves interacting with a floating thin plate. First, in the 1D calculations, the airplanes were B747 and B737. At touch-and-go, when the airplane speed is closer to the water wave speed, even B737 produced large waves based on the resonance. The impacts due to both the touchdown and leaving of the airplanes generated other forward and backward waves. At landing, when the airplane speed approached the water wave speed, a forced wave was generated and amplified, with many free waves ahead. At takeoff, a wave clump, generated shortly after starting to run, propagated in front of the airplanes. Although the wave height increased from superposition with the reflected waves, the wave reflectance was reduced by lowering the flexural rigidity near the airport edge. Second, in the 2D calculations, B787 performed landing and takeoff. When the still water depth is shallower, a grid-like pattern was formed at the floating airport and appeared more remarkably in landing than in takeoff. The effective amplification occurred from a sufficient load applied when the airplane speed approached the water wave speed. Furthermore, the maximum upslope gradient beneath the airplane increased as the still water depth decreased, and it was larger in takeoff than in landing.
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Sieradzki, Adam, Adam Dziubiński und Cezary Galiński. „Performance Comparison of the Optimized Inverted Joined Wing Airplane Concept and Classical Configuration Airplanes“. Archive of Mechanical Engineering 63, Nr. 3 (01.09.2016): 455–70. http://dx.doi.org/10.1515/meceng-2016-0026.

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Abstract The joined wing concept is an unconventional airplane configuration, known since the mid-twenties of the last century. It has several possible advantages, like reduction of the induced drag and weight due to the closed wing concept. The inverted joined wing variant is its rarely considered version, with the front wing being situated above the aft wing. The following paper presents a performance prediction of the recently optimized configuration of this airplane. Flight characteristics obtained numerically were compared with the performance of two classical configuration airplanes of similar category. Their computational fluid dynamics (CFD) models were created basing on available documentation, photographs and some inverse engineering methods. The analysis included simulations performed for a scale of 3-meter wingspan inverted joined wing demonstrator and also for real-scale manned airplanes. Therefore, the results of CFD calculations allowed us to assess the competitiveness of the presented concept, as compared to the most technologically advanced airplanes designed and manufactured to date. At the end of the paper, the areas where the inverted joined wing is better than conventional airplane were predicted and new research possibilities were described.
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A. B. „Paper Airplanes“. Departures in Critical Qualitative Research 7, Nr. 4 (2018): 146–47. http://dx.doi.org/10.1525/dcqr.2018.7.4.146.

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This short poetic response explores my experience performing the play Heavier than Air as a queer teacher; folding my body into these characters, feeling the tensions in the stories, and their resonances with my own. The form of the poem mirrors the process of folding the paper airplanes referenced and used as props throughout the play. As I performed the poem, I folded a paper airplane, and let it take flight on the last line.
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Dissertationen zum Thema "Airplanes"

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Meintjies, Schalk Willem van der Merwe. „Comparative study into occupant support concepts with respect to crash response“. Pretoria : [s.n.], 2004. http://upetd.up.ac.za/thesis/available/etd-01112005-124913.

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Alhayek, Heba. „Airplanes to Nowhere“. Miami University / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=miami1564675215827787.

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MacLeod, James D. (James Donald) Carleton University Dissertation Engineering Aeronautical. „A derivation of gross thrust for a sea-level jet engine test cell“. Ottawa, 1988.

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Pang, Yuen-fai Alson. „Managing aircraft noise /“. Hong Kong : University of Hong Kong, 2002. http://sunzi.lib.hku.hk/hkuto/record.jsp?B2543598x.

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Aronstein, David C. „Effects of rotation on impinging jets for turbine cooling /“. Thesis, Connect to this title online; UW restricted, 1994. http://hdl.handle.net/1773/9985.

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Agenbag, Daniël Sarel. „Longitudinal handling characteristics of a tailless gull-wing aircraft“. Pretoria : [s.n.], 2008. http://upetd.up.ac.za/thesis/available/etd-09182008-132941.

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Schkoda, Ryan F. „Dynamic inversion of underactuated systems via squaring transformation matrix /“. Online version of thesis, 2007. http://hdl.handle.net/1850/5282.

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Brynestad, Mark A. „Investigation of the flight control requirements of a half-scale ducted fan Unmanned Aerial Vehicle“. Thesis, Monterey, Calif. : Naval Postgraduate School, 1992. http://handle.dtic.mil/100.2/ADA252730.

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Thesis (degree of Aeronautical and Astronautical Engineer)--Naval Postgraduate School, March 1992.
Thesis Advisor: Howard, Richard M. "March, 1992." Description based on title screen as viewed on March 10, 2009. Includes bibliographical references (p. 75-76). Also available in print.
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Hall, Zachary Mitchel Ahmed Anwar. „Experimental and computational investigation of a turbofan inlet duct“. Auburn, Ala., 2009. http://hdl.handle.net/10415/1958.

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Kay, Jacob. „Control authority assessment in aircraft conceptual design“. Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-03242009-040703/.

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Bücher zum Thema "Airplanes"

1

Masters, Nancy Robinson. Airplanes. Ann Arbor, Mich: Cherry Lake Pub., 2009.

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Holland, Gini. Airplanes. New York: Benchmark Books, 1996.

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Jean, Allen. Airplanes. North Mankato, Minn: Smart Apple Media, 2003.

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Saunders-Smith, Gail. Airplanes. Mankato, Minn: Pebble Books, 1998.

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Hofer, Charles. Airplanes. New York: PowerKids Press, 2008.

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Steve, Parker. Airplanes. Brookfield, Conn: Copper Beech Books, 1995.

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Masters, Nancy Robinson. Airplanes. Ann Arbor: Cherry Lake Pub., 2008.

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Doman, Mary Kate. Airplanes. Berkeley Heights, NJ: Enslow, 2012.

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Butterfield, Moira. Airplanes. Hauppauge, NY: Barron's, 1999.

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Richardson, Joy. Airplanes. New York: F. Watts, 1994.

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Buchteile zum Thema "Airplanes"

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Kanematsu, Hideyuki, und Dana M. Barry. „Amazing Airplanes“. In Intelligent Systems Reference Library, 65–73. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-19234-5_11.

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Burge, Harriet A. „Airplanes and Infectious Disease“. In The Handbook of Environmental Chemistry, 137–49. Berlin, Heidelberg: Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/b107241.

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Sicha, Choire. „The Problem With Airplanes“. In Never Threaten to Eat Your Co-Workers: Best of Blogs, 101–3. Berkeley, CA: Apress, 2004. http://dx.doi.org/10.1007/978-1-4302-0678-1_25.

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DeLaurier, James. „Canard Airplanes and Biplanes“. In Aircraft Design Concepts, 167–244. Boca Raton: CRC Press, 2022. http://dx.doi.org/10.1201/9781315228167-5.

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Wegener, Peter P. „A Dream Comes True: The Wright Brothers and Their Predecessors“. In What Makes Airplanes Fly?, 1–24. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_1.

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Wegener, Peter P. „Toward High Speed: Supersonic and Hypersonic Flight“. In What Makes Airplanes Fly?, 145–66. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_10.

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Wegener, Peter P. „Air Transportation and the Outlook for the Future“. In What Makes Airplanes Fly?, 167–79. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_11.

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Wegener, Peter P. „Milestones of the Modern Age“. In What Makes Airplanes Fly?, 25–39. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_2.

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Wegener, Peter P. „The Nature of Liquids and Gases“. In What Makes Airplanes Fly?, 41–46. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_3.

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Wegener, Peter P. „The Atmosphere of the Earth“. In What Makes Airplanes Fly?, 47–55. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_4.

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Konferenzberichte zum Thema "Airplanes"

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Nishiyama, Taiga, Daichi Yoshikawa, Nobuhiko Nishio und Kota Tsubouchi. „AirPlanes“. In MobiSys '20: The 18th Annual International Conference on Mobile Systems, Applications, and Services. New York, NY, USA: ACM, 2020. http://dx.doi.org/10.1145/3386901.3396599.

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Molnar, A. „The road from model airplanes to robot airplanes“. In 2009 7th International Symposium on Applied Machine Intelligence and Informatics (SAMI 2009). IEEE, 2009. http://dx.doi.org/10.1109/sami.2009.4956625.

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Hariram, Sham S. „Fire Protection on Airplanes“. In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2005. http://dx.doi.org/10.4271/2005-01-3429.

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Yost, Ralph. „Airplanes Can Be Networked“. In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-2760.

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STOUGH, III, H., DANIEL DICARLO und JAMES PATTON. „Evaluation of airplane spin resistance using proposed criteria for light general aviation airplanes“. In 14th Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2562.

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Kalsi, Swarn S., James Storey, Kent Hamilton und Rodney A. Badcock. „Propulsion motor concepts for airplanes“. In AIAA Propulsion and Energy 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-4517.

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Zubia, Joseba. „Optical Fiber Sensors in Airplanes“. In Optical Sensors. Washington, D.C.: OSA, 2016. http://dx.doi.org/10.1364/sensors.2016.sem4d.3.

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Sheth, Nikhilesh A., und Dennis P. Roach. „Composite Structure Utilization - Commercial Airplanes“. In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2005. http://dx.doi.org/10.4271/2005-01-3315.

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Sikand, Sharanpal (Paul) S., Sham S. Hariram und Darsh Aggarwal. „Fuel Tank Safety on Airplanes“. In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2005. http://dx.doi.org/10.4271/2005-01-3428.

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ROSKAM, J. „Rapid sizing methods for airplanes“. In Aircraft Design Systems and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-4031.

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Berichte der Organisationen zum Thema "Airplanes"

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Faloona, Ian, und Steve Conley. PR-428-123728-R01 Near-Field Natural Gas Dispersion Analysis to Develop an Optimal Airborne Leak Detection. Chantilly, Virginia: Pipeline Research Council International, Inc. (PRCI), August 2017. http://dx.doi.org/10.55274/r0010889.

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The use of airplanes for aerial detection of leaks from gas pipelines presents both great benefits and substantial challenges. Benefits include that typical "entry level" airplanes can easily fly at speeds exceeding 120 miles/hour and, compared to comparable helicopter based leak detection systems, and operate at a small fraction of the cost. However, because airplanes travel faster, requirements for minimum safe altitude are more stringent, limiting "practical" airplane patrols to altitudes more than 490 feet above ground level (AGL). This work evaluates the potential of using fixed wing aircraft to detect plumes from gas leans.
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Harrigan, James. Airplanes and Comparative Advantage. Cambridge, MA: National Bureau of Economic Research, Oktober 2005. http://dx.doi.org/10.3386/w11688.

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Johnk, Robert T., und Arthur R. Camell, Dennis G. Ondrejka. Measurements of shielding effectiveness and cavity characteristics of airplanes. Gaithersburg, MD: National Institute of Standards and Technology, 1994. http://dx.doi.org/10.6028/nist.ir.5023.

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Pratt, Joesph W., Leonard E. Klebanoff, Karina Munoz-Ramos, Abbas A. Akhil, Dita B. Curgus und Benjamin L. Schenkman. Proton Exchange Membrane Fuel Cells for Electrical Power Generation On-Board Commercial Airplanes. Office of Scientific and Technical Information (OSTI), Mai 2011. http://dx.doi.org/10.2172/1219354.

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Curgus, Dita Brigitte, Karina Munoz-Ramos, Joseph William Pratt, Abbas Ali Akhil, Leonard E. Klebanoff und Benjamin L. Schenkman. Proton exchange membrane fuel cells for electrical power generation on-board commercial airplanes. Office of Scientific and Technical Information (OSTI), Mai 2011. http://dx.doi.org/10.2172/1018476.

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6

Löfving, Linnea, Hilma Salonen und Sæunn Gísladóttir. Electric Aviation Outlook in the Nordics. Nordregio, Mai 2023. http://dx.doi.org/10.6027/wp2023:4.1403-2511.

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Annotation:
Regarding geographical accessibility questions, the five Nordic countries stand out in Europe due to their low population density, geographic variety including fjords, lakes, and mountains but also the prominence of sustainable energy sources. Before this backdrop, electric aviation holds the potential to make the region’s transport sector more sustainable while helping to overcome regional development and accessibility challenges, particularly in rural areas. The introduction of electric airplanes in local transport networks promises the reduction inter alia greenhouse gas emissions and air pollution. While several options to achieve zero- or low emission aviation are currently being developed, this report focuses primarily on the electrification of aviation. Yet, electric aircraft still face several technical and economic challenges, including limited range and passenger capacity. Despite these limitations, this working paper highlights a heightened interest in the introduction of electric aviation, exploring the existing situation, challenges and knowledge in the 5 Nordic countries.
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Kosai, M., A. S. Kobayashi und M. Ramulu. Tear Straps in Airplane Fuselage. Fort Belvoir, VA: Defense Technical Information Center, März 1992. http://dx.doi.org/10.21236/ada248543.

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8

Sarrack, A. G. Airplane Crash Frequency for DWPF Structures. Office of Scientific and Technical Information (OSTI), Februar 1995. http://dx.doi.org/10.2172/1482193.

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9

Miess, Joseph C., Reginald C. Murrell und Robert M. Buckanin. Preliminary Airworthiness Evaluation of the RC-12H Airplane. Fort Belvoir, VA: Defense Technical Information Center, Oktober 1987. http://dx.doi.org/10.21236/ada202957.

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10

Kakojima, Hideaki, und Kiyoshi Akinaga. Programmable Flight Control Type Model Airplane for Survey. Warrendale, PA: SAE International, Mai 2005. http://dx.doi.org/10.4271/2005-08-0284.

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