omniomni/omni-engineering huggingface dataset:
USCGC Cape Shoalwater. USCGC Cape Shoalwater was a  type "C"  constructed at the Coast Guard Yard at Curtis Bay, Maryland in 1958 for use as a law enforcement and search and rescue patrol boat.

Design
The Cape class was designed originally for use as a shallow-draft anti-submarine warfare (ASW) craft and was needed because of the increased tension brought about by the Cold War. Cape Shoalwater was a type "C" Cape class and was never fitted with ASW gear because the Coast Guard's mission emphasis had shifted away from ASW to search and rescue by the time she was built. The hull was constructed of steel and the superstructure was aluminum. She was powered by four Cummins VT-600 diesel engines.

History
The Cape class was originally developed as an ASW boat and as a replacement for the aging, World War II vintage, wooden  patrol boats that were used mostly for search and rescue duties. With the outbreak of the Korean War and the requirement tasked to the Coast Guard to secure and patrol port facilities in the United States under the Magnuson Act of 1950, the complete replacement of the 83-foot boat was deferred and the 95-foot boat was used for harbor patrols. The first 95-foot hulls were laid down at the Coast Guard Yard in 1952 and were officially described as "seagoing patrol cutters". Because Coast Guard policy did not provide for naming cutters under  at the time of their construction they were referred to by their hull number only and gained the Cape-class names in 1964 when the service changed the naming criteria to . The class was named for North American geographic capes.

The Cape class was replaced by the   beginning in the late 1980s and many of the decommissioned cutters were transferred to nations of the Caribbean and South America by the Coast Guard.

After commissioning, Cape Shoalwater was assigned a homeport at Mayport, Florida where she was used for law enforcement and search and rescue (SAR) missions. She and her crew earned the Navy Expeditionary Medal for operations relating to the Cuban refugee exodus from 3 January 1961 until 23 October 1962.

In 1963, her homeport was moved to Fort Lauderdale, Florida. On 9 August 1965, she towed the Panamanian motor vessel Seven Seas from  from southeast of Sombrero Key following mutiny aboard the vessel in which three of the crew of Seven Seas had been murdered. The same month, she escorted a Cuban refugee boat from  southwest of Bimini to Port Everglades, Florida. In 1988, the cutter participated in the seizure of the yacht  after marijuana was found on board.

Notes

Citations

References used
 
 
 
 
 
 

1958 ships
Shoalwater
Ships built by the United States Coast Guard Yard
Cape-class cutters of the Royal Bahamas Defence Force
Extempore (software). Extempore is a live coding environment focused on real-time audiovisual software development. It is designed to accommodate the demands of cyber-physical computing. Extempore consists of two integrated languages, Scheme (with extensions) and Extempore Language. It uses the LLVM cross-language compiler to achieve performant digital signal processing and related low-level features, on-the-fly.

Relationship to Impromptu 

Extempore shares the use of Scheme syntax, real-time audiovisual emphasis and lead developer Andrew Sorensen with the older and related project Impromptu.
It runs under both Linux and Mac OS X. The bindings to Apple libraries are absent, but the environment can interface with dynamic libraries.

References

External links 
 

Digital art
Computer programming
Dynamically typed programming languages
Audio programming languages
Music software plugin architectures
Free music software
Electronic music software
Free audio software
Software synthesizers
MacOS multimedia software
Multimedia software for Linux
2011 software
Array programming languages
Live coding
Algorave
SOER. SOER may refer to:

Sustaining Oklahoma's Energy Resources
 Special Operations Engineer Regiment (Australia)
 State and Outlook of Europe's Environment, a report published by the European Environment Agency

See also
Soers
Soer-Varanger
Soer-Trondelag
Seur
 Surface-Oxidation-Enhanced Raman Scattering (SOERS), a Raman spectroelectrochemistry method
Soeur (disambiguation)
Mena station (Arkansas). The Mena Kansas City-Southern Depot is a historic railroad station on Sherwood Street in the center of Mena, Arkansas.  It is long single-story structure, built out of brick, with a tile roof and Mediterranean styling.  It was built in 1920 by the Kansas City Southern Railway to designs by the company architect, T. C. Horstmann, and is one of the most elaborate surviving early-20th century railroad stations in the state.  It is now owned by the city, and houses a local history museum and the local chamber of commerce.

The station was listed on the National Register of Historic Places in 1991.

See also
 Kansas City-Southern Depot (Decatur, Arkansas)
 Kansas City Southern Railway Locomotive No. 73D and Caboose No. 385
 National Register of Historic Places listings in Polk County, Arkansas

References

External links
Depot - City of Mena

Railway stations on the National Register of Historic Places in Arkansas
Railway stations in the United States opened in 1920
Transportation in Polk County, Arkansas
Museums in Polk County, Arkansas
National Register of Historic Places in Polk County, Arkansas
Historic district contributing properties in Arkansas
Former Kansas City Southern Railway stations
Former railway stations in Arkansas
Mediterranean Revival architecture in Arkansas
1920 establishments in Arkansas
Miller–Casella thermometer. The Miller–Casella thermometer was a Six's thermometer with a double bulb used extensively by the Challenger expedition during the late nineteenth century. The thermomemeter was used for water temperature readings along 360 different research stations around the world's oceans.

The thermometer, about  in length, was enclosed in a copper case and filled with a solution of creosote in spirit. A U-shaped mercury tube recorded maximum and minimum temperature as the thermometer was lowered and raised into the ocean. This design assumed accurate measurements could be taken as long as the water closer to the surface of the ocean was always warmer than that below.

Scientists aboard  later questioned this assumption and made temperature measurements with reversing thermometers instead, which wouldn't require the coldest water to be at the ocean's bottom.

References 

Thermometers
Caudron C.21. The Caudron C.21 was a French twin engine biplane built just after World War I, able to carry three passengers in an open cockpit.

Design and development
In 1917 Paul Deville was developing a twin engine observation aircraft when it became clear it would be underpowered and it was therefore not built during World War I. After the war the design, now called the C.21, was completed as a four-seat passenger aircraft.

It was a three bay biplane, with fabric covered, constant chord, unswept wings ending at angled tips. The upper wing, which carried the ailerons, had an 8% greater span and a smaller chord. There was no stagger, so the sets of parallel interplane struts were vertical; flying wires braced each bay. Pairs of V-form engine struts, supporting the two  Le Rhône 9C rotary engines above the lower wing, defined the inner two bays.  There were short, parallel cabane struts from the upper fuselage.

The C.21's fuselage was almost flat sided, with a vertical knife edge at the short nose. It had an open cockpit starting in the extreme nose and seating the three passengers in tandem; the pilot's cockpit was under the trailing edge, with a deep cut-out for better upward vision.  At the rear a straight edged, long and low fin carried a straight edged, balanced rudder that extended down to the keel. An angled tailplane mounted on top of the fuselage had elevators with a cut-out for rudder movement and it had a tailskid undercarriage, with pairs of mainwheels on axles attached to longitudinal bars fixed under the engines on N-form struts.

Operational history

The date of the C.21's first flight is uncertain but it was before February 1919. On 10–11 February it gained publicity with four flights between Paris and Brussels, a distance of  covered in about 140 minutes.  They were flown by Chanteloup, accompanied by designer Deville, to retrieve the passengers from a Caudron C.23, modified into a passenger transport,  which had broken a tailskid at Brussels. The C.21 was advertised in the Caudron catalogue at a price of FF 30,000. It seems only one example was built but its layout was repeated in Caudron's successively larger and more powerful C.22 and C.23 night bombers.

Specifications

References

C.021
1910s French civil aircraft
Biplanes
Rotary-engined aircraft
Aircraft first flown in 1919
Bob Parkinson (aerospace engineer). Robert Charles Parkinson MBE (born 15 July 1941) is a British aerospace engineer who worked on many projects including HOTOL which he cooriginated with Alan Bond.

Dr Parkinson has published numerous papers addressing aspects of advanced aerospace projects; including subjects as diverse as space tethers, space tourism, and reusable launch vehicle architectures.

He was the president of the British Interplanetary Society from 2009 – 2012.

References

1941 births
Living people
People educated at Pate's Grammar School
People from Cheltenham
Rocket scientists
Space programme of the United Kingdom
Members of the Order of the British Empire
Siamack A. Shirazi. Siamack A. Shirazi (born in Iran) is an Iranian-American scientist. He is professor and graduate coordinator of mechanical engineering department at the University of Tulsa, OK, USA. He is fellow of ASME and NACE and currently the Director of Erosion/Corrosion Research Center at University of Tulsa, OK, USA.

Dr. Siamack A. Shirazi is very well known in fluid mechanics integrity management worldwide for SPPS software developed by E/CRC at Tulsa University for particle erosion rate prediction. SPPS has been used widely in erosion threat assessment. He has also published more than hundred peer reviewed journal and conference papers. Siamack received his B.S., M.S. and Ph.D. from the University of New Mexico.

References 

University of Tulsa faculty
Iranian emigrants to the United States
Living people
American mechanical engineers
University of New Mexico alumni
Fellows of the American Society of Mechanical Engineers
Academics from Tulsa, Oklahoma
Year of birth missing (living people)
Ibis GS-501 Urraco. The Ibis GS-501 Urraco (Magpie) is a Colombian homebuilt aircraft that was designed and produced by Ibis Aircraft of Cali, introduced in 2000. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

Design and development
The GS-501 Urraco features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin with vertically-hinged doors, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.

The aircraft is made from sheet aluminium "all-metal" construction, with the wing tips and cowling made from composite material. Its  span wing employs a NACA 650-18m airfoil, mounts flaps and has a wing area of . The wing is supported by V-struts and jury struts. Two wings are available, the SuperSTOL, with double slotted flaps and the Express. The main landing gear is sprung 7075-T6 aluminium, while the nose gear has lever suspension using rubber pucks and helical springs. The main wheels include hydraulic disc brakes.

The acceptable power range is  and the standard engines used are the  Rotax 912ULS and the turbocharged  Rotax 914 powerplant, driving a three-bladed Ivoprop propeller. Continental Motors, Inc. or Lycoming Engines powerplants up to  may also be fitted.

The aircraft has a typical empty weight of  and a gross weight of , giving a useful load of . With full fuel of  the payload for pilot, passenger and baggage is .

The standard day, sea level, no wind, take off with a  engine is  and the landing roll is .

Operational history
By 2010 the company reported that 58 Urracos had been delivered.

Specifications (GS-501 Urraco)

References

External links

GS-501 Urraco
2000s Colombian civil utility aircraft
2000s Colombian ultralight aircraft
Single-engined tractor aircraft
High-wing aircraft
Homebuilt aircraft
UniPhi. UniPhi is a Project management software founded by Mark Heath. UniPhi spun out of mbh management in 2011 following the roll out of AECOM's Global Unite project.

History 

In 2011, UniPhi was introduced to the Global Unite initiative, which involved the implementation of a new client-servicing model. This model captured snapshots of project information from their bespoke cost estimating tools and transferred this data into UniPhi's The Enterprise software. This information then went through a new and improved quality assurance methodology, with UniPhi's software development team building a global data warehouse and analysis services model that would harvest this information to be utilised within any of the 120 offices around the globe. UniPhi's core application was licensed and deployed globally to provide the core architecture of cost plan data capture in a way that enabled portfolio benchmarking. This increased speed to market and generated cost savings.

Another organization that used the software in 2011 was SKM. When the people in charge of the Queensland Flood Recovery road reconstruction program were planning the A$800  million venture, they realized that traditional project management using spreadsheets and Gantt charts would be insufficient.

Types

Web-based 

UniPhi can be used either on the web via desktop computer or through mobile application. The software bundles four main solutions including UniPhi The Enterprise, UniPhi Major Projects, UniPhi Your Business and UniPhi OnSite.

Recognition 

UniPhi was awarded an ABA 100 award in 2014 for innovation for its involvement in the AECOM Global Unite project business award

UniPhi was awarded an ABA 100 award in 2015 and 2017 for product innovation and software innovation respectively.

The Global Unite project won an internal award for innovation at AECOM in 2013

UniPhi was marked as "Companies to Watch" in the weekly Rust Report

Reviews 

The product has been reviewed by:

Google Play, Managing by Project, Rust Report

See also 

 Project Management
 Project management software
 List of project management software
 Comparison of project management software
 Program Management
 Portfolio Management
 Project Portfolio Management

References 

Project management software
Ibis GS-600 Arrow. The GS-600 Arrow is a Colombian homebuilt aircraft that was designed and produced by Ibis Aircraft of Cali, introduced in 2000. When the aircraft was available it was supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

Production has been completed and as of 2011 the aircraft was no longer part of the company's product line.

Design and development
The GS-600 Arrow features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin with vertically-hinged doors, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.

The aircraft is made from sheet aluminium "all-metal" construction, with the wing tips and cowling made from composite material. Its  span wing employs a NACA 650-18m airfoil, mounts flaps and has a wing area of . The wing is supported by V-struts and jury struts. The main landing gear is sprung 7075-T6 aluminium, while the nose gear has lever suspension using rubber pucks and helical springs. The main wheels include hydraulic disc brakes.

The standard engine fitted is the  Rotax 912ULS, driving a three-bladed Ivoprop propeller.

The aircraft has a typical empty weight of  and a gross weight of , giving a useful load of . With full fuel of  the payload for pilot, passenger and baggage is .

Specifications (GS-600 Arrow)

References

External links

GS-600 Arrow
2000s Colombian civil utility aircraft
2000s Colombian ultralight aircraft
Single-engined tractor aircraft
High-wing aircraft
Homebuilt aircraft
Ibis GS-750 Grand Magic. The Ibis GS-750 Grand Magic is a Colombian homebuilt aircraft, designed and produced by Ibis Aircraft of Cali, introduced in 2006. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

Design and development
The GS-750 Grand Magic is a development of the two-seat Ibis GS-700 Magic. It features a strut-braced high-wing, a four-seat enclosed cabin with doors, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.

The aircraft is made from sheet aluminium "all-metal" construction, with the wing tips and cowling made from composite material. Its  span wing employs a NACA 650-18m airfoil, mounts flaps and has a wing area of . The wing is supported by V-struts and jury struts. The main landing gear is sprung 7075-T6 aluminium, while the nose gear has lever suspension using rubber pucks and helical springs. The main wheels include hydraulic disc brakes.

The acceptable power range is  and the standard engines used are the eight cylinder  Jabiru 5100 and, since July 2010, the  Lycoming IO-390-X powerplant.

The aircraft has a typical empty weight of  and a gross weight of , giving a useful load of . With full fuel of  the payload for pilot, passengers and baggage is .

The standard day, sea level, no wind, take off with a  engine is  and the landing roll is .

Operational history
In February 2007 the prototype was delivered to a customer in Ecuador.

Specifications (GS-750 Grand Magic)

References

External links

GS-750 Grand Magic
2000s Colombian civil utility aircraft
Single-engined tractor aircraft
High-wing aircraft
Homebuilt aircraft
Ibis GS-710 Magic. The Ibis GS-710 Magic, also called the GS-450, is a Colombian homebuilt aircraft that was designed and produced by Ibis Aircraft of Cali, developed from the Ibis GS-700 Magic. When it was available the aircraft was supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

Production has been completed and as of 2011 the aircraft was no longer part of the company's product line.

Design and development
The GS-710 Magic was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of .

The aircraft features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin with doors, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.

The GS-710 Magic is made from sheet aluminium "all-metal" construction, with the wing tips and cowling made from composite material. Its  span wing employs a NACA 650-18m airfoil and mounts flaps. The wing employs conventional ailerons or, optionally, Junkers ailerons with leading edge slats and is supported by V-struts with jury struts. The main landing gear is sprung 7075-T6 aluminium, while the nose gear has lever suspension using rubber pucks and helical springs. The main wheels include hydraulic disc brakes.

The standard engine used is the  Rotax 912UL powerplant, driving a three-bladed Ivoprop propeller.

The aircraft's empty weight was reduced by 15% over the GS-700. The GS-710 has a typical empty weight of  and a gross weight of , giving a useful load of . A gross weight of  is optional.

Specifications (GS-710 Magic)

References

External links

GS
2000s Colombian civil utility aircraft
2000s Colombian ultralight aircraft
Single-engined tractor aircraft
High-wing aircraft
Homebuilt aircraft
Ibis GS-730 Super Magic. The Ibis GS-730 Super Magic is a Colombian STOL homebuilt aircraft that was designed and produced by Ibis Aircraft of Cali, introduced in 2007. When it was available the aircraft was supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

Production has been completed and as of 2011 the aircraft was no longer part of the company's product line.

Design and development
The GS-730 Super Magic is a development of the lighter Ibis GS-700 Magic and features a cantilever high-wing with a Robertson STOL kit, a two-seats-in-side-by-side configuration enclosed cabin with doors, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.

The GS-730 Super Magic is made from sheet aluminium "all-metal" construction, with the wing tips and cowling made from composite material. Its  span wing employs a NACA 650-18m airfoil, mounts flaps and has a wing area of . The main landing gear is strengthened and made from 7075-T6 aluminium, while the nose gear has lever suspension using rubber pucks and helical springs. The main wheels include hydraulic disc brakes. Fuel tank capacity is  or optionally  or optionally a maximum of .

The aircraft has a typical empty weight of  and a gross weight of , giving a useful load of . With maximum full fuel of  the payload for pilot, passenger and baggage is .

The standard day, sea level, no wind, take off is  and the landing roll is .

Specifications (GS-730 Super Magic)

References

External links

GS-730
2000s Colombian civil utility aircraft
2000s Colombian ultralight aircraft
Single-engined tractor aircraft
High-wing aircraft
Homebuilt aircraft
Weng Zuze. Weng Zuze (; born January 1941) is a Chinese electrical engineer and academic. He served as president of Hunan University from December 1987 to July 1993. He is a member of the Jiusan Society.

Biography
Weng was born and raised in Shanghai. In 1964 he graduated from Harbin Institute of Technology, where he majored in electrical engineering. Weng joined the chemical engineering faculty of Hunan University in 1978 and was promoted to professor in June 1988. He was a visiting scholar at the University of British Columbia from January 1980 to 1982.

He served as vice-president of Hunan University from December 1985 to December 1987 and the university's president from December 1987 to July 1993.

In December 1989, he joined the Jiusan Society.

References

1941 births
Educators from Shanghai
Living people
Nanyang Model High School alumni
Harbin Institute of Technology alumni
Academic staff of Hunan University
Presidents of Hunan University
Members of the Jiusan Society
Chinese electrical engineers
Engineers from Shanghai