omniomni/omni-engineering huggingface dataset:
Manoharbhai Patel Institute of Engineering and Technology. Manoharbhai Patel Institute of Engineering and Technology (MIET) is a private self-financed technical institution affiliated to University of Nagpur and located in Gondia and Bhandara districts of Maharashtra, India.

Under the management of the former Minister of Civil Aviation (India), Praful Patel, the Institutes's Board of Directors  range from Mukesh Ambani of Reliance to Naresh Goyal of Jet Airways.

History 
The institution have two campus across the Vidarbha region of Maharashtra. The MIET, Gondia in 1983 and MIET, Shahapur, Bhandara in 2010 were established by Gondia Education Society, a private funded education society operating various schools and colleges in the region.

Accredited grade "A" by the Government of Maharashtra. Affiliated to Nagpur University with approval of All India Council of Technical Education (AICTE) and Council of Architecture, New Delhi.

Departments
 Civil Engineering
 Architecture
 Computer Engineering
 Electronics and Communication Engineering
 Information Technology
 Electronics Engineering
 Mechanical Engineering

References

 http://www.mietbhandara.ac.in
 http://www.mietgondia.in

External links
 Official website
 Official website

Engineering colleges in Maharashtra
Bhandara district
Educational institutions established in 2010
2010 establishments in Maharashtra
Gondia district
Educational institutions established in 1983
1983 establishments in Maharashtra
MIET. MIET may refer to:
Member of the Institution of Engineering and Technology

Organisations in Greece 
Cultural Foundation of the National Bank (Greece) (transliteration: Morfotiko Idryma Ethnikis Trapezis)

Organisations in India 
Mahavir Institute of Engineering and Technology, Bhubaneswar, Orissa
Manoharbhai Patel Institute of Engineering and Technology, Shahapur/Gondia, Maharashtra
Model Institute of Engineering and Technology, Jammu, Jammu and Kashmir
Modern Institute of Engineering and Technology, Hooghly, West Bengal

Organisations in Russian Federation 
Moscow Institute of Electronic Technology (currently National Research University of Electronic Technology), Zelenograd, Moscow
Exhibit (web editing tool). Exhibit (part of the SIMILE Project) is a lightweight, structured-data publishing framework that allows developers to create web pages with support for sorting, filtering and rich visualizations. Oriented towards semantic web-type problems, Exhibit can be implemented by writing rich data out to HTML then configuring some CSS and JavaScript code.

Overview
Technically, exhibit is a collection of JavaScript files to be included in a web page. When Exhibit pages are loaded by a web browser, the JavaScript reads in one or more JSON data files and builds a local database in the memory of the machine running the browser. Data can then be filtered and sorted directly in the browser without having to re-query the server. The design of the Exhibit is optimized for browsing faceted data.

The Exhibit code base is currently being developed by members of the SIMILE Project at MIT.

References

External links
Website of the Exhibit Widget
Exhibit Wiki
Official SIMILE Project website

Web development software
Semantic Web
ISO 11992. ISO 11992 (Road vehicles — Interchange of digital information on electrical connections between towing and towed vehicles) is a CAN-based vehicle bus standard by the International Organization for Standardization. It is used for communication between the tractor and one or more trailers.

The protocol structure is similar to SAE J1939. The main differences are timing, bus voltage level, and the structure of the message's 29-bit identifier.

External links

Official texts 
 ISO 11992-1:2019 - Part 1: Physical and data-link layers
 ISO 11992-2:2023 - Part 2: Application layer for brakes and running gear
 ISO 11992-3:2021 - Part 3: Application layer for equipment other than brakes and running gear
 ISO 11992-4:2023 Part 4: Diagnostic communication

11992
Computer buses
Respirocyte. Respirocytes are hypothetical, microscopic, artificial red blood cells that are intended to emulate the function of their organic counterparts, so as to supplement or replace the function of much of the human body's normal respiratory system. Respirocytes were proposed by Robert A. Freitas Jr in his 1998 paper "A Mechanical Artificial Red Blood Cell: Exploratory Design in Medical Nanotechnology".

Respirocytes are an example of molecular nanotechnology, a field of technology still in the very earliest, purely hypothetical phase of development. Current technology is not sufficient to build a respirocyte due to considerations of power, atomic-scale manipulation, immune reaction or toxicity, computation and communication.

Structure of a respirocyte 

Freitas proposed a spherical robot made up of 18 billion atoms arranged as a tiny pressure tank, which would be filled up with oxygen and carbon dioxide.

Uses
In Freitas' proposal, each respirocyte could store and transport 236 times more oxygen than a natural red blood cell, and could release it in a more controlled manner.

Freitas has also proposed "microbivore" robots that would attack pathogens in the manner of white blood cells.

See also 
 Artificial cell
 Biotechnology
 Blood substitute
 Oxycyte
 Synthetic biology

References

External links
Respirocytes at foresight.org

Synthetic biology
Blood cells
Hypothetical technology
Blood substitutes
USS Design (AM-219). USS Design (AM-219) was a steel-hulled Admirable class minesweeper built for the U.S. Navy during World War II. A crew, trained in minesweeping, boarded the new vessel, and proceeded to the Pacific Ocean to clear minefields so that Allied forces could safely invade Japanese-held beaches. For this dangerous work under combat conditions she was awarded three battle stars.

Design was launched 6 February 1944 by Tampa Shipbuilding Co., Tampa, Florida; sponsored by Miss Joan Dall; and commissioned 29 June 1944.

World War II Pacific Theatre operations 
Design sailed from New York 8 September 1944 and escorted a convoy to Pearl Harbor, returning to San Francisco, California, on similar duty 20 November. Three days later she sailed to Seattle, Washington, to pick up another convoy for Pearl Harbor, where she arrived 9 December, en route west.
 
From her arrival at Eniwetok 29 December 1944 until 19 March 1945, Design operated on convoy to and patrol duty at Kossol Roads, Palau; Saipan; Ulithi; Guam; Hollandia, New Guinea; and San Pedro Bay, Leyte.

Pre-invasion minesweeping operations at Okinawa 
Design arrived off Okinawa 26 March for pre-invasion minesweeping, during which she rescued the survivors of YMS-1 class minesweeper YMS-103 which had struck a mine. On 4 July she sailed to sweep in support of the U.S. 3rd Fleet operations against Japan until the last day of the month.

End-of-War operations 
After brief overhaul at San Pedro Bay, Design returned to Okinawa 1 September 1945 and sailed a week later to clear Wakanoura Wan, Honshū, Japan, for occupation landings. She continued to sweep mines off Nagoya, Japan, and in the East China Sea, then departed Sasebo 20 November for the west coast, arriving at San Diego, California, 19 December. On 10 January 1946 she got underway for Galveston, Texas, and Orange, Texas.

Post-War decommissioning 
She was placed in commission in reserve there 14 May 1946 and out of commission in reserve 24 August 1946. She was reclassified MSF-219, 7 February 1955.

Design was stricken at the end of 1960.

Awards 
Design received three battle stars for World War II service.

References 

Blackman, Raymond V. B. Jane's Fighting Ships 1960–61. London: Sampson Low, Marston & Co, 1960.

External links 
 NavSource Online: Mine Warfare Vessel Photo Archive - Design (MSF 219) - ex-AM-219

Admirable-class minesweepers
World War II mine warfare vessels of the United States
Ships built in Tampa, Florida
1944 ships
Henry Potez. Henry Potez  (Méaulte, 30 September 1891 – Paris, 9 November 1981) was a French aircraft industrialist.

He studied in the French Aeronautics School Supaéro. With Marcel Dassault, he was the inventor of the Potez-Bloch propeller which, after 1917, have been set on most of all Allied planes of World War I.

In 1919, he founded his own company, Aviations Potez, that, between the wars, built many planes and seaplanes, in factories which were at that time considered the most modern in the world. He bought the Alessandro Anzani company in 1923. Many Potez planes, such as the Potez 25, 39, 54, 62, 63, were an international success, setting world records.

Over the course of twenty years, 7,000 planes left the production lines. Forty prototypes were designed and more than twenty passed to production - this was remarkable at that time.

In 1936, his factories, considered to be strategic, were nationalised by the French Front populaire government.

After the Second World War, Potez purchased a controlling interest in Air-Fouga who designed and produced the Magister, a two-seat twin engined trainer aircraft, which was a big success.

See also 
 Domaine du Rayol, his villa on the Côte d'Azur

References

French aerospace engineers
Supaéro alumni
1891 births
1981 deaths
Businesspeople in aviation
20th-century French businesspeople
20th-century French inventors
High-throughput computing. In computer science, high-throughput computing (HTC) is the use of many computing resources over long periods of time to accomplish a computational task.

Challenges
The HTC community is also concerned with robustness and reliability of jobs over a long-time scale. That is, being able to create a reliable system from unreliable components. This research is similar to transaction processing, but at a much larger and distributed scale.

Some HTC systems, such as HTCondor and PBS, can run tasks on opportunistic resources. It is a difficult problem, however, to operate in this environment. On one hand the system needs to provide a reliable operating environment for the user's jobs, but at the same time the system must not compromise the integrity of the execute node and allow the owner to always have full control of their resources.

High-throughput vs. high-performance vs. many-task
There are many differences between high-throughput computing, high-performance computing (HPC), and many-task computing (MTC). 

HPC tasks are characterized as needing large amounts of computing power for short periods of time, whereas HTC tasks also require large amounts of computing, but for much longer times (months and years, rather than hours and days). HPC environments are often measured in terms of FLOPS. 

The HTC community, however, is not concerned about operations per second, but rather operations per month or per year. Therefore, the HTC field is more interested in how many jobs can be completed over a long period of time instead of how fast.

As an alternative definition, the European Grid Infrastructure defines HTC as "a computing paradigm that focuses on the efficient execution of a large number of loosely-coupled tasks", while HPC systems tend to focus on tightly coupled parallel jobs, and as such they must execute within a particular site with low-latency interconnects. Conversely, HTC systems are independent, sequential jobs that can be individually scheduled on many different computing resources across multiple administrative boundaries. HTC systems achieve this using various grid computing technologies and techniques.

MTC aims to bridge the gap between HTC and HPC. MTC is reminiscent of HTC, but it differs in the emphasis of using many computing resources over short periods of time to accomplish many computational tasks (i.e. including both dependent and independent tasks), where the primary metrics are measured in seconds (e.g. FLOPS, tasks/s, MB/s I/O rates), as opposed to operations (e.g. jobs) per month. MTC denotes high-performance computations comprising multiple distinct activities, coupled via file system operations.

See also
 Batch processing
 e-Science
 Open Science Grid Consortium
 Grid computing

References

Parallel computing
Advanced Technology College. The Advanced Technology College (ATC) is a four-year technical college located in Daytona Beach, Florida in the United States. This technical college carries courses such as computer technology, construction, manufacturing, engineering, and automotive services.

The ATC is involved in a joint-partnership program with Volusia County and Flagler County school districts. The Advanced Technology Center provides high school students in their junior and senior years the ability to dual-enroll and receive college credits. There is no longer transportation to and from the home high schools to the ATC. The ATC also allows for adult students from Daytona State College to take courses at the ATC.

Notable alumni
Ty Kauffman, writer.

External links
daytonastate.edu Daytona State College Website

Public universities and colleges in Florida
Educational institutions established in 2001
Education in Volusia County, Florida
2001 establishments in Florida
Darmstadt D-18. The Darmstadt D-18 was a German light sports aircraft that was designed and built in the late-1920s by the Akaflieg Darmstadt of the Technische Universität Darmstadt.

Design and development
The aircraft was designed by F. Fecher and students in the aeronautical engineering department of the Technische Universität Darmstadt. It was a development of the D-16 project, that was designed for a sports aircraft contest organized by Idaflieg in 1926. The D-16 design with a 40-horsepower (hp) engine won the first prize, but was not built as the designer decided to strengthen the construction and fit a more powerful 88 hp Armstrong Siddeley Genet radial engine. The result was the D-18, a single aircraft was built in 1929.

The aircraft was a cantilever biplane, with an upper wing placed low above a fuselage and ahead of a lower wing. Particular thought was given to aerodynamics and lightness and the aircraft was small, with a streamlined profile. Initially the D-18 had two open cockpits, but by 1930 it had been modified and fitted with a closed canopy covering both cockpits.

Operational history
The aircraft carried the registration of D-1561. It took part in the Challenge 1929 international tourist plane contest, piloted by Johannes Nehring, being one of the fastest planes in the contest. It was the best aircraft in the fuel consumption trial and, along with two other aircraft, won the first part of the contest - the technical trials. However, the D-18 dropped out due to a forced landing near Września before Poznań on 11 August 1929, during a rally around Europe, because of a fuel pipe clogging. The aircraft turned over and suffered damage; its passenger was injured.

The aircraft was repaired and, now fitted with an enclosed cabin, it took part in another contest, Challenge 1930, again piloted by Rudolf Neininger. On 26 July 1930, during a rally around Europe the D-18 was forced to ditch in the Mediterranean Sea between Barcelona and Nîmes due to breaking a piston. The crew was rescued by a passing ship that also recovered the wreckage.

Specifications

Description
Wooden construction cantilever biplane of extreme stagger. Fuselage oval in cross-section, plywood covered. Single-spar wings, plywood and canvas covered. Aileron on lower wing only Wings were dismounted and folded. Two crew cockpits in tandem, later covered with a  common multi-part canopy. Fixed landing gear with a rear skid. Five-cylinder radial engine in the cowled nose with its cylinders projecting for cooling. Two-blade propeller.

References

Marian Krzyżan: "Międzynarodowe turnieje lotnicze 1929-1934", Warsaw 1988,   (Polish language)

External links

D-18 3-view Akaflieg Darmstadt page
D-18 photo Akaflieg Darmstadt page
Peter M. Bowers, Darmstadt biplanes- article at General Aviation News

1920s German sport aircraft
Akaflieg Darmstadt aircraft
Single-engined tractor aircraft
Biplanes
Aircraft first flown in 1929
1-Hexene (data page). This page provides supplementary chemical data on 1-Hexene.

Material Safety Data Sheet  

The handling of this chemical may incur notable safety precautions. It is highly recommended that you seek the Material Safety Datasheet (MSDS) for this chemical from a reliable source such as SIRI, and follow its directions.

MSDS

Structure and properties

Thermodynamic properties

Spectral data

References 

 Lide, D. R. (Ed.) (1996). CRC Handbook of Chemistry and Physics (76th Edn.). Boca Raton (FL):CRC Press. .
 Spectral Database for Organic Compounds SDBS

Hexene
Chemical data pages cleanup
Darmstadt D-22. The Darmstadt D-22 was a sports-plane of Germany, designed and built by Akaflieg of Technische Universität Darmstadt.

Design and development
The aircraft was designed by F. Fecher in the Akaflieg (academic group of flyers) of Technische Universität Darmstadt. It was a development of Darmstadt D-18, slightly enlarged, more streamlined and fitted with an inline engine. Thanks to strengthening it was better fit to aerobatics. Two were built in 1931.

Just like the D-18, the D-22 was a cantilever biplane, with an upper wing placed low above a fuselage and ahead of a lower wing. Aerodynamic cleanliness and low weight were emphasised in the design, resulting in a small aircraft with clean lines.

Description
The D-22 was of wooden construction with cantilever biplane and oval cross-section fuselage skinned with plywood and fabric on parts of the single-spar wings, which could be dismounted and folded rearwards. The two crew sat in open cockpits in tandem, with windshields. The landing gear was fixed with a rear fuselage skid. The engine was mounted in the fuselage nose and drove a two-bladed fixed-pitch propeller. Fuel was supplied from a  tank in the fuselage.

Operational history
The second aircraft, D-2222, a D-22a, took part in the Challenge 1932 international tourist aircraft contest, piloted by Walter Marienfeld. It was handicapped in technical trials, especially the short landing trial, not having flaps or slats, being relegated to 35th place, from 43 participants, after this section. It improved its score after a rally around Europe, where it took the 4th place, with a cruise speed of . In the maximum speed trial it was beaten only by the five Heinkel He 64s, reaching . As a result, it completed the contest in 17th place. Re-registered as D-EQIN from 1933, it was in use for several years after the Challenges.

Specifications (D-22)

References

Further reading

External links

D-22 photos and drawings at Akaflieg Darmstadt page
 

1930s German sport aircraft
Akaflieg Darmstadt aircraft
Single-engined tractor aircraft
Biplanes
Aircraft first flown in 1931
Pedestrian Accessibility and Movement Environment Laboratory. The Pedestrian Accessibility and Movement Environment Laboratory (PAMELA) was a research facility located in Upper Holloway, part of the University College London in the United Kingdom. 

It was designed to study human interactions in controlled conditions by replicating real-world environments such as urban streets and public parks. The laboratory had an  artificial pavement platform which was used to simulate everyday scenarios, from different types of pedestrians to varying pavement conditions. Its experiments were intended to create safer streets and more user-friendly public spaces.

PAMELA in Upper Holloway was replaced by PEARL (Person-Environment-Activity Research Laboratory) in the London East Business and Technical Park, Dagenham.

See also
 Safety engineering
 NIST stone test wall

References

External links
 
 
 

Pedestrian infrastructure in the United Kingdom
University College London
Buildings and structures in the London Borough of Islington
Udet U 12 Flamingo. The Udet U 12 Flamingo was an aerobatic sports plane and trainer aircraft developed in Germany in the mid-1920s.

Design and development
The U 12 was a conventional, single-bay biplane of wooden construction with the wings braced by large I-struts. The pilot and instructor or passenger sat in tandem, open cockpits. The U 12 proved extremely popular and sold well, due in no small part to Ernst Udet's spectacular aerobatics routines while flying the aircraft. One particularly acclaimed part of his act included swooping down towards the airfield and picking up a handkerchief with the tip of one wing. The popularity of this aircraft was insufficient to rescue Udet Flugzeugbau from its dire financial position, but when the company's assets were taken over by the state of Bavaria to form BFW, production of the U 12 soon resumed in earnest. BFW-built U 12s were exported to Austria, Hungary and Latvia, and later built under licence in these countries as well.

Variants

Germany
 U 12a: main production version with Siemens-Halske Sh 11 engine
 U 12W: float-equipped U 12a (Wasser—"water")
 U 12b: version strengthened for aerobatics and with improved wing design
 U 12c: advanced trainer with reduced wing area
 U 12d: U 12b with Siemens-Halske Sh 12 engine
 U 12e: U 12c with Siemens-Halske Sh 12 engine

Austria
20 aircraft produced by Fliegerwerft Thalerhof
 U 12H: standard U 12a (Holz—"wood")
 U 12S: U 12a with redesigned fuselage of fabric-covered steel tube construction (Stahl—"steel").
 U 12Ö: alternative designation for U 12S (Österreich—"Austria")

Hungary
Forty aircraft produced by KRG and another 40 by Manfred Weiss Works. Some examples armed and used for fighter or bomber training
 Hungária I: similar to U 12a with N-type interplane struts
 Hungária II: similar to U 12a with N-type interplane struts
 Hungária III: similar to U 12a with N-type interplane struts, propeller spinner and Townend ring
 Hungária IV: similar to U 12a. Only Hungarian-built version with I-type interplane struts
 Hungária V: similar to U 12a with N-type interplane struts

Operators
 
 Austrian Air Force (1927–1938)
 
 Royal Hungarian Air Force
 
 Latvian Air Force

 
 Turkish Air Force

Survivors

No original aircraft are known to exist. An airworthy replica was kept at the Deutsches Museum but crashed at the 2013 Tannkosh event.

Specifications (U 12a)

References

 
 
 German aircraft between 1919–1945
 Уголок неба

External links

1920s German civil trainer aircraft
U 12
Aerobatic aircraft
Weiss Manfred aircraft
Biplanes
Single-engined tractor aircraft
Aircraft first flown in 1925
Aircraft with fixed conventional landing gear