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Twisted Wing

Twisted Wing PDF Author: Ruth Newman
Publisher: Simon and Schuster
ISBN: 1849830509
Category : Fiction
Languages : en
Pages : 308

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.

Twisted Wing

Twisted Wing PDF Author: Ruth Newman
Publisher: Simon and Schuster
ISBN: 1849830509
Category : Fiction
Languages : en
Pages : 308

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.

An Investigation of the Effects of a Geometric Twist on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing-body Configuration at Transonic Speeds

An Investigation of the Effects of a Geometric Twist on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing-body Configuration at Transonic Speeds PDF Author: Claude V. Williams
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 92

Book Description


Transonic and Supersonic Wind-tunnel Tests of Wing-body Combinations Designed for High Efficiency at a Mach Number of 1.41

Transonic and Supersonic Wind-tunnel Tests of Wing-body Combinations Designed for High Efficiency at a Mach Number of 1.41 PDF Author: Frederick C. Grant
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 86

Book Description


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

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 PDF Author: Harold I. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60

Book Description


The Elastic Twist of Straight Wings for Symmetrical Load Conditions

The Elastic Twist of Straight Wings for Symmetrical Load Conditions PDF Author: Walther Gustav Carl Boccius
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 68

Book Description


Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds

Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds PDF Author: Frederick C. Grant
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 18

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).

Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 48

Book Description


Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962

Book Description


Drag Due to Lift at Mach Numbers Up to 2.0

Drag Due to Lift at Mach Numbers Up to 2.0 PDF Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

Book Description