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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.
SAP Composite Application Framework (SAP CAF) is a composition tool in NWDS (SAP NetWeaver Developer Studio, an Eclipse-based IDE) and runtime on SAP Web Application Server Java for developing, testing, deploying, running and configuring composite applications. It is tightly integrated in the NetWeaver stack and is currently the tool of choice ...
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The An-2 can take off and land on unsurfaced airstrips. (Photo taken at Kunmadaras military airbase, Hungary.) An-2 on skis at Volosovo air field, [11] Chekhovsky District, Moscow region An-2 at Grand Junction aviation show. The An-2 is a mass-produced single-engine biplane that was deliberately furnished with a minimum of complex systems. The ...
ACS 2: Audio control system ACU 1: Air condition unit ACU 2: Alternator control unit [2] Protection from alternator over-voltage. AD Airworthiness Directive: ADA Advisory area ADAHRS Air data attitude heading reference system ADC Air data computer: ADD Acceptable deferred defect ADF Automatic direction finder: Navigation equipment ADI Attitude ...
SAP also developed a graphical user interfaceor GUI. For the next 12 years, SAP dominated the large business applications market. It was successful primarily because it was flexible. Because SAP was a modular system (meaning that the various functions provided by it could be purchased piecemeal) it was a versatile system.
For example the form above, simplified slightly by putting C L0 = 0, has a maximum C L /C D at C L 2 = C D0 /K. For a propeller aircraft this is the maximum endurance condition and gives a speed of 185 km/h (115 mph). The corresponding maximum range condition is the maximum of C L 3/2 /C D, at C L 2 = 3.C D0 /K, and so