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TAF VIII-2, four-seater Tandem Airfoil Flairboat Typ Jörg II, built in 1983. Following the F&E and test period, Dipl. Ing. Günther Jörg was awarded with the "Phillip Morris Scientific Award" for the Transportation System for the future. Another TAF VIII-2, built in 1994 was given to a Japanese private citizen.
Ekranoplan A-90 Orlyonok. A ground-effect vehicle (GEV), also called a wing-in-ground-effect (WIGE or WIG), ground-effect craft/machine (GEM), wingship, flarecraft, surface effect vehicle or ekranoplan (Russian: экранопла́н – "screenglider"), is a vehicle that is able to move over the surface by gaining support from the reactions of the air against the surface of the earth or water.
The Pro version adds support for VST, Audio Unit, and LADSPA plugins, among other features. Other software by Rogue Amoeba includes Nicecast, Airfoil, and Fission. Nicecast combines Audio Hijack's ability to capture audio with the open source Icecast streaming media system to enable users to broadcast audio from any program over the internet.
The Fouga CM.170 Magister was developed to perform both basic and intermediate training activities. [8] It is a compact, tandem seat aircraft with performance akin to larger, more powerful aircraft.
Differences between the CUH-11 and CUH-12 series included a reduction in rated power from 250 W to 230 W, a reduction in weight from 2.8 to 2.5 kg, and physical buttons. [3] [4] [5] The CUH-12xx series are also referred to as the "C chassis" variant of the PS4. [6] In late June 2015, a 1 TB CUH-11 series machine was announced for European/PAL ...
Furthermore, a Free Wake Vortex model was implemented for the accurate representation of the near and far wake of the turbine. A new version of QBlade was released in August 2022. QBlade Community Edition (QBlade-CE 2.0.4) includes all functionality that is required for the aero-servo-hydro-elastic simulation of wind turbines.
[8] [17] The spin is deliberately initiated, and its recovery is precise and without delay. [18] [17] The SZD-54-2 has well-balanced controls and moderate control forces. [19] In a thermal, the glider circles and centres steadily. [16] The sailplane accelerates quickly with the NN-8 airfoil and achieves a glide ratio of 42 in the 20-metre version.
In February 1976, work commenced to automate the methods contained in the USAF Stability and Control DATCOM, specifically those contained in sections 4, 5, 6 and 7.The work was performed by the McDonnell Douglas Corporation under contract with the United States Air Force in conjunction with engineers at the Air Force Flight Dynamics Laboratory in Wright-Patterson Air Force Base.