Supersonic

Supersonic
Author: Oasis
Publisher: Hachette UK
Total Pages: 440
Release: 2021-10-14
Genre: Biography & Autobiography
ISBN: 1472285468

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'An entertaining first-hand account of pure rock 'n' roll madness.' The Daily Telegraph 'Hundreds of exclusive photos and brilliant one-liners make for a sensational read.' the Sun 'We are the biggest band in Britain of all time, ever. The funny thing is, all that fucking mouthing off three years ago about how we were going to be the biggest band in the world - we actually went and did it.' Noel Gallagher Oasis are one of the biggest bands the world has ever seen. Here, in Supersonic, they tell the story of their beginnings from dive-bar hopefuls to global superstars. They themselves talk us through the pivotal moments in their phenomenal trajectory, from the day Noel Gallagher joined his brother Liam's band, through their first crucial five years culminating at their landmark gigs at Knebworth Park in 1996 - the pinnacle of their success. With over thirty hours of interviews with Liam, Noel and those closest to them, this book documents in unprecedented depth and with their trademark candour and humour, the story behind one of the world's greatest bands, all told in their own words and fully illustrated with exclusive photographs and ephemera throughout.

Supersonic Cruise Technology

Supersonic Cruise Technology
Author: F. Edward McLean
Publisher:
Total Pages: 208
Release: 1985
Genre: Technology & Engineering
ISBN:

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"This document provides a historic perspective of supersonic cruise technology, beginning with the early NACA supersonic research and including efforts during the B-70 and SST phase. It also records technological progress made in the NASA SCR and VCE programs." -- Foreward.

Supersonic Transports

Supersonic Transports
Author: United States. Flight Standards Service
Publisher:
Total Pages: 136
Release: 1961
Genre: Supersonic transport planes
ISBN:

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Supersonic

Supersonic
Author: Lawrence Azerrad
Publisher:
Total Pages: 0
Release: 2025-03-04
Genre: Design
ISBN: 9783791393629

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This stylishly illustrated book looks back at the future of air travel and is as sleek and elegant as the Concorde aircraft it celebrates - now in an enlarged edition. When the first commercial Concorde flights zoomed off the runways in Paris and London in the late 1960s, crossing the Atlantic in just under three hours, they established a new standard for luxury flight. Powered by 38,000 pounds of thrust and easily recognizable with its delta wing and drooping nose, the Concorde jet embodied the pinnacle of aviation technology and industrial design. It quickly became the preferred mode of transatlantic flight for superstars and business moguls alike. Opening with a lively history of the jet and how it changed travel, the book focuses on the look and feel of the Concorde. Photos of the jet's evolving interiors show how the original, starkly designed cabin gave way to luxury seats and interiors designed by the likes of Raymond Loewy, Sir Terence Conran and Andrée Putman. Filled with fascinating historical and technical background, and drawn from the author's personal collection of more than one thousand Concorde-related objects, this elegant book offers rarely seen historical photography and firsthand contributions from the people who helped create the Concorde experience from take-off to landing and beyond.

Commercial Supersonic Technology

Commercial Supersonic Technology
Author: National Research Council
Publisher: National Academies Press
Total Pages: 128
Release: 2002-01-16
Genre: Technology & Engineering
ISBN: 0309183383

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High-speed flight is a major technological challenge for both commercial and business aviation. As a first step in revitalizing efforts by the National Aeronautics and Space Administration (NASA) to achieve the technology objective of high-speed air travel, NASA requested the National Research Council (NRC) to conduct a study that would identify approaches for achieving breakthroughs in research and technology for commercial supersonic aircraft. Commercial Supersonic Technology documents the results of that effort. This report describes technical areas where ongoing work should be continued and new focused research initiated to enable operational deployment of an environmentally acceptable, economically viable commercial aircraft capable of sustained supersonic flight, including flight over land, at speeds up to approximately Mach 2 in the next 25 years or less.

Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations
Author: Adriana Nastase
Publisher: Elsevier
Total Pages: 425
Release: 2010-07-07
Genre: Technology & Engineering
ISBN: 008055699X

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Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. Computational work and experimental results show the real-world application of computational results Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations Includes a fully optimized and integrated design for a proposed supersonic transport aircraft

The Aerodynamic Design of Supersonic Propellers from Structural Considerations

The Aerodynamic Design of Supersonic Propellers from Structural Considerations
Author: Jerome B. Hammack
Publisher:
Total Pages: 682
Release: 1952
Genre: Aerodynamics, Supersonic
ISBN:

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The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.

Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds

Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds
Author: Robert T. Taylor
Publisher:
Total Pages: 22
Release: 1961
Genre: Aerodynamics, Supersonic
ISBN:

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An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of paraglider models at moderate to high supersonic speeds. The models were deployed from a sting in the supersonic stream and steady-state aerodynamics performance data were obtained. Maximum values of the lift-drag ratio were about 1.4 at a Mach number of 2.65 and about 1.2 at a Mach number of 4.65. The angles of attack over which the models could be flown were limited by unsteady behavior of the canopy.