omniomni/omni-engineering huggingface dataset:
Government Polytechnic Jhansi. The Government Polytechnic Jhansi is a college affiliated with the Uttar Pradesh Board of Technical Education, India. Its principal is Naveen kumar, and it is situated on Gwalior road near the Kanpur barrier. There are five engineering courses at the college: Electronics Engineering, Mechanical Engineering (auto), Mechanical Engineering (pro), Civil Engineering, and Electrical Engineering.

On the 'Karam BhumiI ' of Maharani Laxmi Bai, popularly known as 'Jhansi Ki Rani' the foundation of the polytechnic was laid down in 1958. The institute is situated on the Jhansi Gwalior Road. Jhansi the head of 'Bundelkhand' region is an historical and industrial city. The institute started its academic session in the disciplines of Civil, Electrical and Mechanical Engineering. In 1971 the institute started a diploma course in Automobile Engineering, in 1972 a diploma course in Electronics Engineering and in 1993 a diploma in Computer Applications. The annual intakes are 30, 30,30,40,30 and 40 respectively.

The Diploma certificate is given by the Board of Technical Education, U.P Lucknow.

The institute has an administrative building, an academic building, hostel, N.C.C blocks, and playground.

It is situated at Gwalior Road Jhansi near Asharam Ashram. The distance from the railway station and bus stand is 5 km

External links 

 Official website

Technical universities and colleges in Uttar Pradesh
Education in Jhansi
1958 establishments in Uttar Pradesh
Educational institutions established in 1958
Lalbhai. Lalbhai is a name of Indian origin. Notable people with the name include:

Lalbhai Dalpatbhai (1863-1912), Indian industrialist
Kasturbhai Lalbhai (1894-1980), Indian industrialist
Umedram Lalbhai Desai (1868-1930), Indian medical doctor
Arvind Narottambhai Lalbhai (1918-2007), Indian industrialist

See also
Lalbhai Dalpatram College of Engineering, Indian engineering college
Lalbhai Dalpatbhai Museum, Indian museum
Barking Town Urban District Council Light Railways. Barking Town Urban District Council Light Railways operated a passenger tramway service in Barking between 1903 and 1929.

History

Barking Town Urban District Council opened services on this tramway on 1 December 1903. With a total of 2.8 route miles, this was one of the shortest tramway operations in Britain.

The depot was located at

Fleet

1-3 Brush Electrical Engineering Company 1903
4-5 Brush Electrical Engineering Company 1903 (withdrawn in 1926)
6-7 Brush Electrical Engineering Company 1903
8 Brush Electrical Engineering Company 1911 (sold to Ilford Urban District Council Tramways in 1915)
9 Brush Electrical Engineering Company 1911 (sold to East Ham Corporation Tramways in 1915)
10 Brush Electrical Engineering Company 1912 (sold to Ilford Urban District Council Tramways in 1914)

Closure

On 16 February 1929 the last services were replaced by buses.

References

Tram transport in England
Trams in London
Indian Institute of Nano Science & Technology. Indian Institute of Nano Science & Technology  (IINSc) is a research institution that teaches nano science and technology. It is located in Bangalore, India.

History
Karnataka is home to many such initiatives..and for Indian Institute of Nano Science & Technology to support and develop nanotechnology and reap the benefit of technology. Nanotechnology in India has started to noticed and high potential, develop and get importance in both research and commercial value.

In  Karnataka research centres like Jawaharlal Nehru Centre for Advanced Scientific Research Centre, Indian Institute of Science and the National Centre for Biological Sciences are main research institutes which support the nano park initiative.

The focus of the Indian Institute of Nano Science & Technology will be research and development of nano materials.

Nano Park is the first of its kind in India and supports the development of medical devices, diagnostic kits and pharmaceuticals.

Campus
Karnataka state government initiated to set Nano Park in Bangalore with estimated budget allocation of Rs. 150 Crores .
The park spreads 25 acres of land and building  at Tumakur Road Bangalore. The Park will be on similar lines of an Information Technology Park.

Main building
The infrastructure would include a science and technology business incubator which will nurture early stage entrepreneurial ventures based on nano science and technology. There will be laboratories and clean rooms that will prove conducive for nano research.

See also

References

External links

Research institutes in Bengaluru
Scientific organisations based in India
Science and technology studies associations
Year of establishment missing
Swift Aircraft Swift. The Swift Aircraft Swift is a single engine, conventional light aircraft, seating two in side-by-side configuration.  It is being developed in the UK but has yet to fly.

Design and development

The Swift is mostly built from composite materials; flying surfaces and the fuselage are formed from composite sandwiches and the wing and tailplane have carbon fibre spars. It has a low wing of trapezoidal plan with slightly upturned tips, fitted with Frise ailerons and slotted flaps. The rear surfaces are also trapezoidal.  There is a trim tab in the elevator and a ground adjustable tab on the rudder.

The cockpit has a fixed windscreen and rearward-sliding canopy and is equipped with dual controls. There is a baggage space behind the side-by-side seats.  The Swift has a fixed, tricycle undercarriage with the mainwheels on fuselage mounted, spring steel, cantilever legs. The mainwheels have disc brakes and the nosewheel is steerable.  The Swift is designed to accept a range of Textron Lycoming horizontally opposed engines in the power range , driving a three-bladed propeller.

The Swift program was announced in May 2009. In 2015 Swift Technology Group announced a "multi million pound investment" supporting development of the aircraft and other products, and exhibited a static display at AeroExpo UK.

In 2021, the Royal Air Force announced its intention to become carbon neutral, called Project MONET. To further this project, the UK MOD awarded a contract in 2023 to develop the Swift as a zero-emission aircraft with a possible implementation date of 2027. Swift Technology Group have begun experimenting with hemp and flax fibres in the composite panels, as well as alternate fuels, and even electric propulsion.

Variants
Swift II Intended to be type certified to EASA CS-23
Swift M260 Military version of above, which may replace the Grob Tutor T1 in No. 6 Flying Training School RAF
Swift LSA Intended to be certified to EASA CS-LSA
Swift VLA Intended to be certified to EASA CS-VLA in kit and factory-complete flyaway versions

Specifications (Swift II)

References

External links
 Swift Aircraft

Proposed aircraft of the United Kingdom
USS Omaha (LCS-12). USS Omaha (LCS-12) is an  of the United States Navy. She is the fourth ship to be named for Omaha, the largest city in Nebraska. The vessel's keel was laid down on 18 February 2015 at the Austal USA shipyard in Mobile, Alabama and launched on 20 November. The ship was commissioned at San Diego, California on 3 February 2018 and was assigned to Littoral Combat Ship Squadron One.

Design
In 2002, the United States Navy initiated a program to develop the first of a fleet of littoral combat ships. The Navy initially ordered two trimaran hulled ships from General Dynamics, which became known as the  after the first ship of the class, . Even-numbered U.S. Navy littoral combat ships are built using the Independence-class trimaran design, while odd-numbered ships are based on a competing design, the conventional monohull . The initial order of littoral combat ships involved a total of four ships, including two of the Independence-class design. On 29 December 2010, the Navy announced that it was awarding Austal USA a contract to build ten additional Independence-class littoral combat ships.

Construction and career
The vessel was ordered from Austal USA with a contract awarded on 29 December 2010. The ceremonial laying of the keel was on 18 February 2015, at their shipyard in Mobile, Alabama.
Omaha was launched from Austal USA's shipyards in Mobile, Alabama on 20 November 2015. Omaha was christened on 19 December 2015.  The ship's sponsor was Omaha philanthropist Susie Buffett. The littoral combat ship was the fourth ship to be named for Omaha, the largest city in Nebraska. Omaha was commissioned on 3 February 2018 in San Diego, California. She was assigned to Littoral Combat Ship Squadron One.

UFO incident 
On 15 July 2019 alleged multiple UFOs were tracked on the ship's radar while training off the coast of San Diego. Subsequent investigation by the Pentagon's Unidentified Aerial Phenomena Task Force (UAPTF) failed to determine the nature or origin of the phenomena, which remain unexplained.

References

External links
 

2015 ships
Independence-class littoral combat ships
Finsterwalder Funfex. The Finsterwalder Funfex is a German high-wing, single-place, hang glider, designed and produced by Finsterwalder.

Design and development
The Funfex and the smaller-sized Airfex are intended as man-packable double-surface intermediate gliders for recreational cross-country flying. As such the Funfex weighs only  and can be reduced to a folded size of 

The aircraft is made from aluminum tubing, with the wing covered in Dacron sailcloth. Its  span wing is cable braced from a single kingpost. The nose angle is 120° and the aspect ratio is 5.5:1.

Variants
Airfex
Medium-sized glider with wing area of  and a pilot hook-in weight of . DHV certified as Class 1-2.
Funfex
Large-sized glider with wing area of  and a pilot hook-in weight of . DHV certified as Class 2.

Specifications (Funfex)

References

External links

Hang gliders
Finsterwalder Perfex. The Finsterwalder Perfex is a German high-wing, single-place, hang glider, designed and produced by Finsterwalder.

Design and development
The Perfex and the smaller sized Lightfex are intended as man-packable single-surface beginner gliders for recreational flying. As such the Perfex weighs only  and can be reduced to a folded size of 

The aircraft is made from aluminum tubing, with the wing covered in Dacron sailcloth. Its  span wing is cable braced from a single kingpost. The nose angle is 120° and the aspect ratio is 5.5:1.

Variants
Lightfex
Medium sized glider with wing area of  and a pilot recommended weight of . DHV certified as Class 2.
Perfex
Large sized glider with wing area of  and a pilot recommended weight of . DHV certified as Class 1-2.

Specifications (Perfex)

References

External links

Hang gliders
Finsterwalder Speedfex. The Finsterwalder Speedfex is a German high-wing, single-place, hang glider, designed and produced by Finsterwalder.

Design and development
The Speedfex was designed as man-packable double-surface competition glider for cross country flying. As such the Speedfex weighs only  and can be reduced to a folded size of 

The aircraft is made from aluminum tubing, with the wing covered in Dacron sailcloth. Its  span wing is cable braced from a single kingpost. The nose angle is 130° and the aspect ratio is 7.1:1. The pilot hook-in weight range is . The glider is certified as DHV Class 2.

Specifications (Speedfex)

References

External links

Hang gliders
Carlos Ruiz Fuller. Carlos Enrique Ruiz Fuller (September 23, 1916 – March 28, 1997) was a Chilean geologist and mining engineer noted for his planning and direction of the Institute of Geological Investigations of Chile and his pioneering surveying and mapping of Chile's metal deposits in the 1960s. He was also the head of the geology sector of the Production Development Corporation (CORFO) and undersecretary at the Ministry of Mining of Chile between 1954 and 1957.

The mineral carlosruizite was named after him in 1994.

References

1916 births
1997 deaths
20th-century Chilean geologists
University of Chile alumni
RFA Wave Conqueror. RFA Wave Conqueror was a Wave-class fleet support tanker of the Royal Fleet Auxiliary that was built in 1943, as SS Empire Law by the Furness Shipbuilding Company, Haverton Hill, United Kingdom.

She saw service during the Korean War and was scrapped in 1960.

References

1943 ships
Empire ships
Wave-class oilers
Ships built on the River Tees
Finsterwalder. Finsterwalder GmbH is a German aircraft manufacturer specializing in hang gliders, paragliders and related accessories. The company is headquartered in Munich.

Most of the company's hang glider designs are intended to be folded down to a small size for man-packing up mountains.

Finsterwalder GmbH is made up of two divisions. The headquarters is in Munich and focuses on hang glider design, production and repair along with helmet design and production. Charly Products is located in Seeg and produces paragliders, harnesses and rescue systems.

History
The company was formed in 1974 by Thomas Finsterwalder as a kayak design and production enterprise. The first hang glider designed and produced was the Finsterwalder Bergfex (), which weighed  and could be broken down in 8 minutes to a package  long for ground transport.

In 1985 the factory and all equipment were destroyed by a fire, delaying production until the following year.

In 1990 the company bought out Charly Products adding paragliders and parachute systems to the company line. Since the take-over the company has done business as Finsterwalder & Charly. In 1994 Charly started a partnership with Nova Paragliders.

Aircraft

References

External links

Aircraft manufacturers of Germany
Hang gliders
Paragliders
Flight Design Axxess. The Flight Design Axxess is a German high-wing, single-place, rigid-wing hang glider that was designed and produced by Flight Design.

Production is complete and the aircraft is no longer available.

Design and development
The Axxess was intended as a high-performance rigid-wing hang glider for competition use. The early production versions had flaps but these were later deleted, as they offered no performance advantage.

The wing structure includes a carbon D-spar, with the wing covered in Dacron sailcloth. The foldable design of the ribs allow for a small packing size. Its  span wing has a nose angle of 165° and the aspect ratio is 12.7:1, with flaps retracted the aspect ratio changed to 13.6:1. The maximum takeoff weight range is . In 2003 the aircraft sold for €7241.

The glider was German DHV 3E certified on 20 November 2002.

Specifications (2003 model Axxess)

References

Axxess
Hang gliders
Flight Design Exxtacy. The Flight Design Exxtacy is a German high-wing, single or two-place, rigid-wing hang glider that was designed and produced by Flight Design.

Production is complete and the aircraft is no longer available.

Design and development
The Exxtacy was intended as a high-performance rigid-wing hang glider, for competition use and two-place instruction.

The Exxtacy wing is based upon a carbon-fiber-reinforced polymer cantilever box spar, with ribs and wing tips, also of the same material. Control is by weight-shift, with roll control augmented by wing top-surface spoilers. For thermalling flight and landing, inboard flaps were installed. The aircraft achieves a glide ratio of 17.5:1.

The aircraft can be dismantled for ground transport and folds to  x  x .

Variants
Exxtacy 13.5
Single place model. Its  span wing has a nose angle of 165° and the aspect ratio is 9.4:1. The pilot hook-in weight range is . In 2003 the aircraft sold for €6078. Certified as DHV Class 3.
Exxtacy Biplace
Two place model. Its  span wing has a nose angle of 165° and the aspect ratio is 10.05:1. The pilot hook-in weight range is . In 2003 the aircraft sold for €6509. Certified as DHV Class 3.

Aircraft on display
Deutsches Museum Flugwerft Schleissheim

Specifications (2003 model Exxtacy 13.5)

References

Exxtacy
Hang gliders
Aerochia LT-1. The Aerochia LT-1 is a single place, composite construction, homebuilt aircraft.

Design and development

The LT-1 was co-developed by Andy Chiavetta, a composite parts specialist, and air racer, Darryl Greenamyer. The intent was to design a very simple homebuilt aircraft for first-time builders.

The LT-1 is a single seat, low-wing, composite aircraft with tricycle landing gear. The wing uses an elliptical planform.

The first flight was performed in May 2010 piloted by Len Fox.

Specifications (LT-1)

References

Homebuilt aircraft
Statampere. The statampere (statA) is the derived electromagnetic unit of electric current in the CGS-ESU (electrostatic cgs) and Gaussian systems of units.:278
One statampere corresponds to / ampere ≈  in the SI system of units. 

The name statampere is a shortening of abstatampere, where the idea was that the prefix abstat  should stand for absolute electrostatic and mean ‘belonging to the CGS-ESU (electrostatic cgs) absolute system of units’.

The esu-cgs (or "electrostatic cgs") units are one of several systems of electromagnetic units within the centimetre–gram–second system of units; others include CGS-EMU (or "electromagnetic cgs units"), Gaussian units, and Heaviside–Lorentz units. In the cgs-emu system, the unit of electric current is the abampere. The unit of current in the Heaviside–Lorentz system doesn't have a special name.

The other units in the cgs-esu and Gaussian systems related to the statampere are: 

 statcoulomb – the charge that passes in one second through any cross-section of a conductor carrying a steady current of one statampere
 statvolt – the electrostatic potential difference such that moving a charge of one statcoulomb through it at constant speed requires one erg of work to be done.
 statohm – the resistance of a conductor that, with a constant current of one statampere through it, maintains between its terminals a potential difference of one statvolt

Notes

References

Units of electric current
Centimetre–gram–second system of units
Nicholas-Beazley NB-3. The Nicholas-Beazley NB-3, or Barling NB-3, is a two-seat, training aircraft of the 1920s.

Design
The Barling NB-3 was designed by Walter Barling in 1927. The aircraft was advertised as being able to right itself from any position with hands off the controls and also as being spin-proof. The NB-3 is a low-wing, tandem-seat, open-cockpit aircraft with conventional landing gear. The fuselage was constructed of welded chrome-moly steel tubing with aircraft fabric covering. The wings used a unique double-layered corrugated aluminum skin with a smooth exterior that required custom presses to handle the various thicknesses of material along the span. The center section was straight with dihedral in the outer bays. The spar was also aluminum with a U-shaped profile. The aircraft was powered by an Anzani 3-cylinder radial engine, Superior radial or LeBlond 60-5-D. The main gear used long struts attached to the upper fuselage for the largest landing gear geometry. The NB-3 fuselage was widened, giving one cockpit a side-by-side seating arrangement to accommodate three people. The new aircraft was named the NB-4.

Operational history
The NB-3 was test flown by Claude Sterling in February 1929. The plane competed in the 1929 National Air Races, placing first or second in events in its class. The Marshall Flying School advertised the NB-3 as a one-day-to-learn-to-fly aircraft with students flying in the morning, an aerodynamics class, learning how to weld by mid-afternoon, salesmanship, and a leisure round of boxing and swimming by evening. Ruth Alexander established a new world record for altitude in 1930 using an NB-3 over San Diego, California. A NB-3 is on display at the N-B plant's hometown airport in Marshall, Missouri.

Variants
NB-3
 Anzani powered - 3 built
NB-3G
Armstrong-Siddely Genet Mk II 
NB-3L 
Lambert 
NB-3V
 Velie M-5  1 built
NB-4G
 Side-by-side variant with Armstrong-Siddely Genet Mk II 
NB-4L 
 Side-by-side variant with Lambert . ATC#365 issued 12-13-1930
NB-4W 
Side-by-side variant with Warner . ATC#386 issued 12-13-1930

Specifications (NB-3)

References

External links
image of a NB-3

1920s United States civil utility aircraft
Low-wing aircraft
Aircraft first flown in 1928
Single-engined tractor aircraft
Sree Buddha College of Engineering, Elavumthitta. Sree Buddha College of Engineering is a self-financing engineering college under Sree Buddha Foundation, Kollam. This college is located in Elavumthitta of Pathanamthitta District and is affiliated to APJ Abdul Kalam Kerala Technological University. Sree Buddha College of Engineering, Pattoor (Alapuzha District), Sree Buddha Central School, Karunagappally and Sree Buddha Central School, Pattoor are some of the Centres of Excellence Associated by the Foundation. Currently, there are four engineering streams in this college: Electrical and electronics engineering, Civil Engineering, Computer Science, Mechanical Engineering & Electronics and Communication Engineering.

Courses 
 B.Tech.
 M.Tech.

B.Tech 
 Electronics and Communication Engineering (ECE)
 Computer Science and Engineering (CSE)
 Civil Engineering (CE)
 Electrical and Electronics Engineering (EEE)
 Mechanical Engineering (ME)

M.Tech 
 Communication Engineering (ECE)
 Computer Science and Engineering (CSE)
 Computer Aided Structural Engineering (Civil)

References

External links

Engineering colleges in Kerala
Universities and colleges in Pathanamthitta district
Educational institutions in India with year of establishment missing
Akaflieg Darmstadt D-39. The Akaflieg Darmstadt D-39 was a single-seat motor glider derived from the D-38 sailplane. Built in Germany in the late 1970s, it was not intended for production and only one was constructed.

Design and development
The D-39 was a motorised version of the D-38 sailplane, with wings moved down from the latter's shoulder-wing position to the bottom of the fuselage. A Limbach SL 1700 flat four engine was conventionally mounted in the nose; the propeller could be removed but not folded away in flight.  The wings, with 4° of dihedral, tail and monocoque fuselage were formed from glass fibre balsa sandwiches and the ailerons from glass fibre/Klégécel foam sandwiches. The D-38 had an all moving T-tailplane, fitted with a Flettner tab.  It landed on a retractable monowheel, fitted with a drum brake and assisted by a small, fixed tailwheel.

The D-39 was first flown on 28 June 1979.  By July 1982 it had been modified into the D-39b, with a greater span, revised wing roots and fitted with two-bladed Hoffmann Propeller airscrew and three pitch positions. 
The „D-39HKW“
was developed on the fuselage of the D-39, using 20-Meter flapped wing V

Variants
D-39 Original version
D-39b Same aircraft modified with greater span, revised roots and a new propeller.

Specifications (D-39)

References

Motor gliders
1970s German sailplanes
Akaflieg Darmstadt aircraft
Single-engined tractor aircraft
Low-wing aircraft
Aircraft first flown in 1979
Martin N2M. 

The Martin N2M was a prototype American primary training biplane, built for the United States Navy by the Glenn L. Martin Company. It was never accepted by the Navy and only the prototype was built.

The prototype was designated N2M-1 by the United States Navy, and it first flew in 1924. The N2M-1 was based on the Martin 66 Night Mail and was a biplane powered by a  Wright-Hisso E-4 engine. It had two open cockpits in tandem for a crew of two.

Specifications

See also

References

Notes

Bibliography

 

N2M
1920s United States military trainer aircraft
Single-engined tractor aircraft
Biplanes
Aircraft with fixed conventional landing gear
Single-engined piston aircraft