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Browsing by Supervisor "Howe, D."

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Aircraft design optimisation conceptual evaluation of a three-lifting surface turbo-fan airliner

Basto Nunes, J. M. (Cranfield University, 1995-02)

Today's high competitiveness in the airline industry urges for the development of even more efficient transport aircraft. In many cases lower operating costs are the key to survival. Although the introduction of emerging ...
Composite faced sandwich construction for primary spacecraft structures

Slade, R. (Cranfield University, 1989-09)

This study investigated the application of fibre reinforced composite materials to spacecraft sandwich structures. In particular, aspects of the manufacture, analysis and design optimisation of components fabricated using ...
Design of aerobatic aircraft wing

Potter, J. G. (Cranfield University, 1969-05-19)

The aircraft under consideration in the following text is a swing wing, 50,000 lb. (maximum weight), land based strike aircraft. The various roles of the aircraft are strike operations at a Mach number of 2.0 and height ...
A design study for a compound helicopter featured with a convertible prop/rotor

Mostafa, A. (Cranfield University, 1989-10-30)

A compound helicopter is a hybrid vehicle, fundamentally a helicopter. It uses an auxiliary lift and propulsion device(s) in order to eliminate the lifting rotor high speed limitation of retreating blade stall effects, ...
Failure of Laminated Fibre-reinforced Composite Structures Subject to Combined Loadings

Nahas, Mahmoud Nadim (Cranfield University, 1980)

A new modified maximum strain failure criterion is proposed to predict the failure of the laminae of laminated fibre-reinforced composite structures when the laminate is subjected to combined loadings. The new criterion ...
The minimum weight design of compression structures including plasticity effects

Richards, D. M. (Cranfield University, 1977-11)

The minimum weight design of a wide range of structures required to resist compressive loading is considered. Items which have been analysed in detail include struts of various sorts, thin plates, honeycomb ...
Multi-disciplinary design of wings for transport aircraft operating at high subsonic speed

Djafri, Demil Y. (Cranfield University, 1995-12)

In this thesis a methodology for designing wings for transport aircraft operating at high subsonic speed is investigated. Several methods are studied, including more accurate methods such as the computational methods. ...

Browsing by Supervisor "Howe, D."

Browsing by Supervisor "Howe, D."

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