Twisted Wing
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Author |
: Ruth Newman |
Publisher |
: Simon and Schuster |
Total Pages |
: 308 |
Release |
: 2010-02-18 |
ISBN-10 |
: 9781849830508 |
ISBN-13 |
: 1849830509 |
Rating |
: 4/5 (08 Downloads) |
Synopsis Twisted Wing by : Ruth Newman
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 |
: |
Total Pages |
: 92 |
Release |
: 1954 |
ISBN-10 |
: UOM:39015086465682 |
ISBN-13 |
: |
Rating |
: 4/5 (82 Downloads) |
Synopsis An Investigation of the Effects of a Geometric Twist on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing-body Configuration at Transonic Speeds by : Claude V. Williams
Author |
: Frederick C. Grant |
Publisher |
: |
Total Pages |
: 86 |
Release |
: 1960 |
ISBN-10 |
: UIUC:30112106689315 |
ISBN-13 |
: |
Rating |
: 4/5 (15 Downloads) |
Synopsis Transonic and Supersonic Wind-tunnel Tests of Wing-body Combinations Designed for High Efficiency at a Mach Number of 1.41 by : Frederick C. Grant
Author |
: Harold I. Johnson |
Publisher |
: |
Total Pages |
: 60 |
Release |
: 1953 |
ISBN-10 |
: UOM:39015086465054 |
ISBN-13 |
: |
Rating |
: 4/5 (54 Downloads) |
Synopsis Investigation of Three Tapered 45© Sweptback Cambered and Twisted Wings Covering a Simultaneous Variation in Aspect Ratio and Thickness Ratio and of One Related Symmetrical Wing at Transonic Speeds by the Wing-flow Method by : Harold I. Johnson
Author |
: Walther Gustav Carl Boccius |
Publisher |
: |
Total Pages |
: 68 |
Release |
: 1948 |
ISBN-10 |
: UOM:39015104977502 |
ISBN-13 |
: |
Rating |
: 4/5 (02 Downloads) |
Synopsis The Elastic Twist of Straight Wings for Symmetrical Load Conditions by : Walther Gustav Carl Boccius
Author |
: Frederick C. Grant |
Publisher |
: |
Total Pages |
: 18 |
Release |
: 1957 |
ISBN-10 |
: UOM:39015086466110 |
ISBN-13 |
: |
Rating |
: 4/5 (10 Downloads) |
Synopsis Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds by : Frederick C. Grant
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 |
: United States. National Advisory Committee for Aeronautics |
Publisher |
: |
Total Pages |
: |
Release |
: 1955 |
ISBN-10 |
: STANFORD:36105024166121 |
ISBN-13 |
: |
Rating |
: 4/5 (21 Downloads) |
Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author |
: United States. National Advisory Committee for Aeronautics |
Publisher |
: |
Total Pages |
: 48 |
Release |
: 1951 |
ISBN-10 |
: STANFORD:36105024789898 |
ISBN-13 |
: |
Rating |
: 4/5 (98 Downloads) |
Synopsis Report by : United States. National Advisory Committee for Aeronautics
Author |
: |
Publisher |
: |
Total Pages |
: 962 |
Release |
: 1955 |
ISBN-10 |
: MINN:31951D00028207H |
ISBN-13 |
: |
Rating |
: 4/5 (7H Downloads) |
Author |
: Edward C. Polhamus |
Publisher |
: |
Total Pages |
: 28 |
Release |
: 1953 |
ISBN-10 |
: UOM:39015086490334 |
ISBN-13 |
: |
Rating |
: 4/5 (34 Downloads) |
Synopsis Drag Due to Lift at Mach Numbers Up to 2.0 by : Edward C. Polhamus