Author: Ruth Newman
Publisher: Simon and Schuster
ISBN: 1849830509
Category : Fiction
Languages : en
Pages : 308
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Book Description
Cambridge is home to 18,000 students, 1,500 academics - and one serial killer. The discovery of the headless, mutilated body of a female undergraduate in her bloodsoaked college room heralds the start of a series of bizarre and extremely violent murders. For the students of Ariel College, a siege mentality has developed following weeks of media interest in the 'Cambridge Butcher'. University life has become not about surviving their exams, but surviving full stop. Forensic psychiatrist Matthew Denison is sure that his traumatised patient, student Olivia Coscadden, has the killer's identity locked up in her memory. That within the little clique she belonged to lurks someone with a grudge. Someone who has yet to finish settling their score. In order to get to the truth, Denison must delve into the secrets hidden within Olivia's subconscious. Secrets that are about to lead him into a nightmare beyond imagining.
Author: Claude V. Williams
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 92
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Book Description
Author: Frederick C. Grant
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 86
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Book Description
Author: Harold I. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
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Book Description
Author: Walther Gustav Carl Boccius
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 68
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Book Description
Author: Frederick C. Grant
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 18
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Book Description
Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been tested in the Mach number range from 0.8 to 2.0. The test results showed, in general, rather good agreement with theoretical predictions of the incremental span loadings due to twist for zero angle of attack. The measured incremental span loadings due to twist generally diminished with increasing angle of attack through the Mach number range. At a Mach number of 0.9, the incremental loadings progressively vanished from the tip inboard with increasing angle of attack. For the highest angles of attack (about 20 degrees) at Mach number 0.9, there was no difference in the span loadings of the flat and twisted wings. At a higher supersonic speeds, a similar vanishing at the tips of the incremental loading due to twist was starting at the highest angles of attack (near 20 degrees).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 344
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 424
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Book Description
Chiefly translations from foreign aeronautical journals.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 348
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Book Description
Chiefly translations from foreign aeronautical journals.
Author: F. Schultz-Grunow
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 516
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Book Description
From measurements in the free boundary layer of a plate the laws governing the velocity distribution and a new resistance law are derived which, by increasing Reynolds number Re(sub x) afford lower resistance values than the logarithmic law. The transverse velocities, the shearing stress, and the mixing path profiles were also defined.
