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Dallara was contracted by Beppe Lucchini to design a car for his new BMS Scuderia Italia racing team, which was to participate in the 1988 Formula One season. The F188, powered by a Cosworth DFZ V8 engine, [ 2 ] was designed by Giampaolo Dallara in conjunction with Sergio Rinland . [ 1 ]
By its introduction at the 1954 French GP the 2,496 cc (152.3 cu in) (76.0×68.8 mm) desmodromic valves straight 8 M 196 R delivered 256 PS (188 kW). The M 196 was the only F1 engine with direct fuel injection, giving it a considerable advantage over the other carburetted engines.
The 30th edition (1996) was renamed CRC Standard Mathematical Tables and Formulae, with Daniel Ian Zwillinger as the editor-in-chief. [2] The 33rd edition (2018) was renamed CRC Standard Mathematical Tables and Formulas. [3]
An F1 car can be no more than 200 cm wide and 95 cm tall. [1] Though there is no maximum length, other rules set indirect limits on these dimensions, and nearly every aspect of the car carries size regulations; consequently the various cars tend to be very close to the same size. The car and driver must together weigh at least 798 kg as of 2024 ...
The Benetton B188 is a Formula One racing car designed by Rory Byrne and raced by Benetton team in the 1988 Formula One season and in the first half of the 1989 Formula One season. Dating back to when the team started as Toleman in 1981, the B188 was the first car produced by the team not to be powered by a turbocharged engine.
4-Amino-2,2,6,6-tetramethyl-4-piperidine is an organic compound with the formula H 2 NCH(CH 2 CMe 2) 2 NH (where Me = CH 3). Classified as a diamine , it is a colorless oily liquid. The compound is an intermediate in the preparation of Bobbitt's salt , an oxidant used in organic synthesis.
6 ft 2 in (188 cm) [1] Bowers's amateur-built airplane design, the Fly Baby A Bowers Bi-Baby , this is the Fly Baby with the optional upper wing installed. Peter M. Bowers (May 15, 1918 – April 27, 2003) was an American aeronautical engineer, airplane designer, and a journalist and historian specializing in the field of aviation .
a=chord, b=thickness, thickness-to-chord ratio = b/a The F-104 wing has a very low thickness-to-chord ratio of 3.36%. In aeronautics, the thickness-to-chord ratio, sometimes simply chord ratio or thickness ratio, compares the maximum vertical thickness of a wing to its chord.