enow.com Web Search

Search results

1. Results from the WOW.Com Content Network

2. Propelling nozzle - Wikipedia

   en.wikipedia.org/wiki/Propelling_nozzle

   At subsonic speeds, the airflow constricts the exhaust to a convergent shape. When afterburning is selected and the aircraft speeds up, the two nozzles dilate, which allows the exhaust to form a convergent-divergent shape, speeding the exhaust gasses past Mach 1. More complex engine installations use a tertiary airflow to reduce exit area at ...

3. Honda J engine - Wikipedia

   en.wikipedia.org/wiki/Honda_J_engine

   The J30A4 pushed output to 242 hp (180 kW) and 212 lb⋅ft (287 N⋅m) using a three-way VTEC system, a higher (10.0:1) compression ratio and a novel exhaust manifold cast as one piece with the cylinder head. It weighs nearly 20 lb (9.1 kg) less and is an inch shorter than J30A1.

4. RD-0126 - Wikipedia

   en.wikipedia.org/wiki/RD-0126

   The RD-0126 "Yastreb" (РД-0126 «Ястреб») was a liquid-fuel cryogenic rocket engine burning liquid hydrogen and liquid oxygen, developed by KBKhA Kosberg in Voronezh, Russia.

5. Barel Graal - Wikipedia

   en.wikipedia.org/wiki/Barel_Graal

   Data from World Directory of Leisure Aviation 2003–04 and Company website General characteristics Crew: one Length: 6 m (19 ft 8 in) Wingspan: 15.00 m (49 ft 3 in) Wing area: 10 m 2 (110 sq ft) Aspect ratio: 22.5:1 Airfoil: Eppler E668 Empty weight: 200 kg (441 lb) Gross weight: 300 kg (661 lb) Fuel capacity: 12 litres (2.6 imp gal; 3.2 US gal) Powerplant: 1 × RDM 200 twin cylinder engine ...

6. CFM International CFM56 - Wikipedia

   en.wikipedia.org/wiki/CFM_International_CFM56

   CFMI tested both a mixed and unmixed exhaust design at the beginning of development; [4] most variants of the engine have an unmixed exhaust nozzle. [nb 2] Only the high-power CFM56-5C, designed for the Airbus A340, has a mixed-flow exhaust nozzle. [nb 1] [53] GE and Snecma also tested the effectiveness of chevrons on reducing jet noise.

7. Rolladen-Schneider LS8 - Wikipedia

   en.wikipedia.org/wiki/Rolladen-Schneider_LS8

   LS8-a: as the previous –a model except the spar is not reinforced for span extension. LS8-s: corresponds to the previous LS8-18 model, with a larger main undercarriage, the wing further reinforced for an increased maximum weight of 575 kg in the 18m mode and other minor changes. (11 built, together with LS8-st)