Erscheinungsdatum: 28.01.2013, Medium: Taschenbuch, Einband: Kartoniert / Broschiert, Titel: Airplane Characteristics. a Systematic Introduction for Flyer and Student and for All Who Are Interested in Aviation, Autor: Bedell, Frederick B., Verlag: HardPress Publishing, Sprache: Englisch, Schlagworte: HISTORY // General, Rubrik: Geschichte, Seiten: 152, Informationen: 423:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on White w/Matte Lam, Gewicht: 214 gr, Verkäufer: averdo
Erscheinungsdatum: 05/2008, Medium: Taschenbuch, Einband: Kartoniert / Broschiert, Titel: Aerodynamic Analysis of A Landing Transport Airplane in Windshear, Titelzusatz: Estimation of Windshear Profile, Dynamic Ground Effect, and Stability and Control Characteristics of a Twin-Jet Transport Airplane, Autor: Weng, Chin-Tang Tom // Lan, Chuan-Tau Edward, Verlag: VDM Verlag, Sprache: Englisch, Rubrik: Technik // Sonstiges, Seiten: 120, Informationen: Paperback, Gewicht: 195 gr, Verkäufer: averdo
Selection and training for the Army's Glider Pilot Regiment was both vigorous and thoroughly demanding. GPR veterans recall their experience of training to be members of one of the British Army's new elite regiments. Once they had survived the initial toughening up, it was on to elementary fixed-wing flying with the RAF and then on to gliding in a variety of aircraft including the Horsa Glider. Using an exact full-size replica of the Horsa Glider built at RAF Shawbury, the team gain an insight into the construction, size and flying characteristics of this iconic airplane. Veterans explain how the aircraft handled and the controls they used in their five mile glide from six thousand feet. The operations of the Glider Pilot Regiment are covered from the first small scale attempt to destroy the German Heavy Water plant in Norway through to the near disastrous first major commitment at night to the invasion of Sicily in July 1943.Special Features:Range of Diagrams, interviews with GPR veterans.
Erscheinungsdatum: 12.10.2018, Medium: Taschenbuch, Einband: Kartoniert / Broschiert, Titel: Comparison of Yaw Characteristics of a Single-Engine Airplane Model With Single-Rotating and Dual-Rotating Propellers (Classic Reprint), Autor: Neely, R. H., Verlag: Forgotten Books, Sprache: Englisch, Schlagworte: TECHNOLOGY & ENGINEERING // Automotive, Rubrik: Maschinenbau // Fertigungstechnik, Seiten: 70, Informationen: 23:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on White w/Gloss Lam, Gewicht: 108 gr, Verkäufer: averdo
Airplane Characteristics; a Systematic Introduction for Flyer and Student and for All Who Are Interested in Aviation ab 12.49 € als Taschenbuch: . Aus dem Bereich: Bücher, Taschenbücher, Geist & Wissen,
Biologically inspired self-organization methods can help to manage the access control to the shared communication medium of Wireless Sensor Networks. One lightweight approach is the primitive of desynchronization, which relies on the periodic transmission of short control messages - similar to the periodical pulses of oscillators. This primitive of desynchronization has already been successfully implemented as MAC protocol for single-hop topologies. Moreover, there are also some concepts of such a protocol for multi-hop topologies available. However, the existing implementations may handle just a certain class of multi-hop topologies or are not robust against topology dynamics. In addition to the sophisticated access control of the sensor nodes of a Wireless Sensor Network in arbitrary multi-hop topologies, the communication protocol has to be lightweight, applicable, and scalable. These characteristics are of particular interest for distributed and randomly deployed networks (e.g., by dropping nodes off an airplane).
The book deals with the conceptual design and LCC estimation concepts of very light airplane (VLA), very light business jet (VLJ) and unmanned air system (UAS). The greatest part of the results can be useful also for all other aeronautical products. The work consists of four main parts. The first one is a brief introduction to the innovative and brand new segment represented by the light aircraft. The second part consists of a detailed description of a new conceptual design method. It is a statistical model, which allows to calculate structure and systems weights, the main geometric characteristics of the wing and the fuselage and the airplane performance. The study of Life Cycle Cost (LCC) estimation is entirely described in chapter 4 of the book. A wide variety of pre-existing methods are discussed. In order to generate a unique LCC estimating tool, the standard methods are integrated with new models and CERs,. The last section illustrates some models applications, which are intended to validate the estimating methodology. The examples concern two of the most representative very light jets: the Eclipse 500 and the ATG Javelin.
High Quality Content by WIKIPEDIA articles! Airport 1975 is a 1974 disaster film and the first sequel to the successful 1970 hit Airport. The movie is one among many of a class of Disaster films that became a movie-going craze during the 1970s. Its plot devices and characterizations, including a singing nun (Helen Reddy), a former glamorous star (Gloria Swanson as herself), an alcoholic (Myrna Loy), a child in need of an organ transplant (Linda Blair) and a chatterbox (Sid Caesar) were parodied in 1980's Airplane!. The characteristics of Airport 1975 were also used in numerous similar films to come, including the film's sequels Airport '77 and The Concorde...Airport '79. Though derided by the critics upon its release, Airport 1975 was ultimately a success. With a budget of US$4 million, the film made over US$47 million at the box office. Helen Reddy was nominated for a Golden Globe Award for Most Promising Newcomer - Female. The film was included, however, in the popular book The Fifty Worst Films of All Time three years later in 1978.
Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. The Zlin Z-50 is a aerobatic sports plane built by the Czechoslovakian company Zlin Aircraft.In autumn 1973 it was decided in Moravan Otrokovice to develop a new single seat aerobatic airplane. The design team was headed by Jan Mikula, a noted Czech designer. During the design phase, computer optimization was used to achieve the desired aerodynamic characteristics. The principal goal was to determine the optimum engine and propeller combination for this aircraft. Designers settled on the Lycoming AIO-540 D4B5 horizontally-opposed six-cylinder piston engine, rated at 194 kW (260 HP), driving a three-blade Hartzell constant speed propeller.