krainaksiazek aerodynamic components of aircraft at high speeds 20107063

- znaleziono 3 produkty w 2 sklepach

Cancelled aircraft projects - 2838787360

119,36 zł

Cancelled aircraft projects Books LLC, Reference Series

Książki / Literatura obcojęzyczna

Source: Wikipedia. Pages: 101. Chapters: Avro Canada CF-105 Arrow, FMA IAe 33 Pulqui II, Boeing 2707, Miles M.52, Fairey Rotodyne, Boeing Skyfox, Avro Canada C102 Jetliner, Bristol Brabazon, Vickers V-1000, Nanchang Q-6, DFS 346, Fairchild Dornier 728 family, Heinkel He 176, OMAC Laser 300, Eclipse 400, IAI Lavi, Project Sabre II, Saunders-Roe Princess, FMA SAIA 90, Embraer/FMA CBA 123 Vector, Helwan HA-300, Convair Model 118, McDonnell Douglas MD-12, Tupolev Tu-334, Douglas Cloudster II, Westland Westminster, Adam A700, RTAF-5, Piper PA-47 PiperJet, Shenyang J-13, OKB-1 EF 140, Fairchild Dornier 428JET, Beechcraft Model 34, I.Ae. 30 Ńancú, Boeing Sonic Cruiser, Baade 152, Yakovlev Yak-16, FFA P-16, AVE Mizar, VisionAire Vantage, Douglas DC-8, LearAvia Lear Fan, BAC Two-Eleven and Three-Eleven, Burnelli CBY-3, RWD-18, EFW N-20, Douglas DC-4E, Shanghai Y-10, Tupolev Tu-70, Ilyushin Il-18, Novi Avion, Bisnovat 5, Aichi S1A, EADS Mako/HEAT, Fokker F26, PZL-230 Skorpion, CMC Leopard, Mitsubishi Ki-33, Nakajima Ki-12, Kawasaki Ki-28, Cierva CR Twin, Kawasaki Ki-5, Nakajima Ki-11, Lockheed Saturn, Blohm & Voss BV 144, R102, Fokker F.XXIV, Fokker F.V, Britten Sheriff, Chengdu J-9, Bristol Tramp, Cessna 620, FMA I.Ae. 37, FMA I.Ae. 27 Pulqui I, Armstrong Whitworth AW.171, AD Seaplane Type 1000, Short S.32, Austin Kestrel, ZSO 523, Let L-610, Sukhoi-Gulfstream S-21, Boeing 7J7, Lockheed Excalibur, Nakajima Ki-8, Auster Atlantic, Saab 36, List of cancelled military projects, Fairey FC1, Dassault AVE Grand Duc, Saunders-Roe Duchess, Avtek 400, Avocet ProJet, Rocketplane XP, Aerial Distributors Distributor Wing, Caproni Ca.60, Cunliffe-Owen Concordia, IAR 95, Aviation Traders Accountant, PZL I-22 Iryda, Boisavia Anjou, Ayres LM200 Loadmaster, Sud-Ouest Triton, AIDC XC-2, Cessna 187, Cessna 160, ATG Javelin, Aceair AERIKS 200, Atlas Carver, Capelis XC-12, VFW-Fokker H3, Aero A.24, Ahrens AR 404, Indonesian Aerospace N-2130, Mil Mi-X1, ANF Les Mureaux 160T, ANF Les Mureaux 140T, Ilyushin Il-108, McDonnell Douglas MD-94X, Saab 38, Beechcraft Model 16, Boeing New Large Airplane, Embraer MFT-LF, High Speed Civil Transport, CNNA HL-2, CNNA HL-8. Excerpt: The Avro Canada CF-105 Arrow was a delta-winged interceptor aircraft, designed and built by Avro Aircraft Limited (Canada) in Malton, Ontario, Canada, as the culmination of a design study that began in 1953. Considered to be both an advanced technical and aerodynamic achievement for the Canadian aviation industry, the CF-105 held the promise of Mach 2 speeds at altitudes exceeding 50,000 ft (15,000 m), and was intended to serve as the Royal Canadian Air Force's primary interceptor in the 1960s and beyond. Not long after the 1958 start of its flight test program, the development of the Arrow (including its Orenda Iroquois jet engines) was abruptly and controversially halted before the project review had taken place, sparking a long and bitter political debate. The controversy engendered by the cancellation and subsequent destruction of the aircraft in production, remains a topic for debate among historians, political observers and industry pundits. "This action effectively put Avro out of business and its highly skilled engineering and production personnel scattered... The incident was a traumatic one... and to this day, many mourn the loss of the Arrow." Full size replica of the CF-105 Arrow at the Canadian Air and Space Museum, TorontoIn the post-Second World War period, the Soviet Union began developin...


Turbulent Transonic Flow Phenomena Influence on Aeroelastic Stability - 2834700622

366,72 zł

Turbulent Transonic Flow Phenomena Influence on Aeroelastic Stability LAP Lambert Academic Publishing

Książki / Literatura obcojęzyczna

The new aircraft developments seem to aim at flexible and high aspect ratio wings, flying at high altitudes and transonic cruise Mach numbers. Considering these structural and aerodynamic conditions, the non-linear effects cannot be neglected. In the present work, the aerodynamic non-linear effects at transonic speeds are evaluated upon the aeroelastic stability point of view. CFD techniques are used to obtain a pair of aerodynamic coefficients time history for both pitch and plunging structural DOFs. Dual-time Stepping, SA turbulence model, CFL constant and multigrid algorithms are incorporated in the solution. In addition, two types of mesh movement algorithms are used and compared. In addition, author proposed a CFL number correction, when using multigrid strategy, and an algebraic algorithm for unstructured aerodynamic mesh generation. The resultant CFD time signal is treated in the Laplace domain. Its correspondent AIC matrix is aproximated by a rational function. The resultant AIC matrix is incorporated in the linear coupled system of equations of motion written in modal form. The coupled aeroelastic system is solved using state space variables.


Cougar 140mm Vortex HDB CF-V14H - 1990966825

105,90 zł

Cougar 140mm Vortex HDB CF-V14H Cougar

kategoria nadrzedna nie istnieje

Cougar's first fan series "Vortex" does not only look great, it also has "power under the hood" When a new fan comes to the market, and the data sheet of the fan shows that many new patents were integrated and that this performance piece comes from Cougar, it becomes clear that this fan series is truly great! The design, as always with components from Cougar, is exceptionally beautiful. The black / orange design gives the fan a unique look. This almost makes installing this fan in an enclosure a pity. The technology in this fan is also rather exceptional: A truly impressive airflow at low speeds and exceptionally low noise emissions leave the competition far behind. How the developers managed to achieve all this is hard to put in words, so simply have a look at the data sheet. Special features: HIGH-VORTEX AIRFLOW, patented fan and frame design High air flow at extremely low noise levels PATENTED FAN BLADE DESIGN Innovative fan blade design ensures focussed air flow and optimal cooling ANTI-VIBRATION PADS Reduces all vibration to a minimum AERODYNAMIC DESIGN The aero-dynamic fan shape reduces vortexing Technical specifications: Dimensions: 140x140x25mm Colour: Black frame, orange fan blades Nominal voltage: 12V Nominal speed: 1200rpm (+/- 10%) Airflow: 119,8m


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