document

TU Delft Aula Conservation Management Plan

de Jonge, W. (author), Clarke, Nicholas (author), Kerkhoven, C.W. (author)

A Conservation Management Plan (CMP) for governing, managing, maintaining and eventual changes of the Aula Building at the Delft University of Technology, aimed at optimizing the balance between the value as a listed national monument and the value for daily use of the building.<br/>The CMP provides advice to all parties concerned, based on...

report 2023

document

KaDEr | rEflectie: Eindrapportage KaDEr Gelderland project | fase 1 en 2 | 2017 - 2021

Zijlstra, H. (author), Quist, W.J. (author), Nijhuis, S. (author), Clarke, Nicholas (author)

Final report of the research project KaDEr

report 2022

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Experimental Manoeuvring Data of Tanker "British Bombardier"

Journee, J.M.J. (author), Clarke, D. (author)

report 2005

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The manual steering criterion based upon phase margin

Clarke, David (author), Cox, Chris (author), Fox, Pat (author)

report 1993

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Numerical Computation of Two-Dimensional Unsteady Detonation Waves in High Energy Solids

Clarke, J.F. (author), Karni, S. (author), Quirk, J.J. (author), Simmonds, L.G. (author), Toro, E.F. (author)

We are concerned with theoretical modelling of unsteady, two-dimensional detonation waves in high energy solids. A mathematical model and a numerical method to solve the associated hyperbolic system of equations are presented. The model consists of the Euler equations augmented bby extra conservation laws and source terms to accoxint for...

report 1990

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Numerical studies of a detonation analogue

Clarke, J.F. (author), Roe, P.L. (author), Simmonds, L.G. (author), Toro, E.F. (author)

Starting in 1946 as the College of Aeronautics, the Cranfield Institute of Technology was granted university status in 1969. In 1993 it changed its name to Cranfield University.

report 1987

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Dynamic Behaviour of Combustible Gases Between a Shock Wave and a Following Flame

Clarke, J.F. (author), Wang, Z.W. (author)

The paper describes events in time intervals up to the appearance of re-ignition of a combustible gas in the induction domain between a strong precursor shock wave and a following premixed flame. The re-ignition process takes place immediately ahead of the flame, and involves both local temperature and local pressure increases which are strongly...

report 1986

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Quasi-steady flames on an evolving atmosphere

Clarke, J.F. (author)

Theoretical studies of pre-mixed flames are complicated by the fact that the atmosphere ahead of the combustion wave is essentially in a state of disequilibrium. Various devices have been proposed to overcome this difficulty and this paper proposes, and examines, a model that admits from the outset that the basic atmosphere will be undergoing...

report 1984

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A review of theories currently being used to model steady plane flames on flame-holders

McIntosh, A.C. (author), Clarke, J.F. (author)

The stability of burner flames for arbitrary Lewis number is considered on the basis of large activation energy modelling. Previous leading-order-only approaches are now extended to second order in 0,-1 (the inverse activation energy). The assumption that the unsteady perturbations are small (order E) means that one must discuss the...

report 1983

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Second order theory of unsteady burner-anchored flames with arbitrary Lewis Number

McIntosh, A.C. (author), Clarke, J.F. (author)

Three theoretical models of plane flames burning on a cooled porous-plug type of flame-holder are reviewed and compared with experimentally observed relationships between stand-off distance, flame speed and temperature. It is shown that for most practical burners their conductance is large and that for near adiabatic conditions, the order of the...

report 1983

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Non-Steady Gas Dynamic Effects in the Induction Domain Behind a Strong Shock Wave

Clarke, J.F. (author), Cant, R.S. (author)

Processes in the region between a driving piston or contact surface and a strong shock wave (e.g. Mach number > 1.5) can be modelled theoretically as relatively small-perturbation events. The combustion reaction is assumed to be of simple irreversible Arrhenius type; perturbations are then of the order of the dimensionless inverse activation...

report 1982

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The Application of Manoeuvring Criteria in Hull Design Using Linear Theory

Clarke, D. (author), Gedling, P. (author), Hine, G. (author)

report 1982

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Manoeuvring trials with the 193.000 Tonne deadweight tanker Esso Bernicia

Clarke, David (author), Patterson, D.R. (author), Wooderson, R.K. (author)

report 1972

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A re-analysis of the steering trials on th 50.000 ton D.W. tanker British Bombardier

Clarke, David (author)

report

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A two-dimensional strip method for surface ship hull derivatives Comparison of theory with experiments on a segmented tanker model

Clarke, David (author)

report

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Liquid velocity measurement by electronic detection of particle images

Clarke, William B. (author)

report 1968

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Fluid velocity measurement by doppler shift of scattered light

Clarke, William B. (author)

report 1968

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Manoeuvring Trials with the 50.000-ton Deadweight Tanker British Bombardier Part 2: Steering

Clarke, David (author)

report 1966

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Analogue computer simulation of the steering and manoeuvring characteristics of a mariner class vessel

Clarke, David (author)

report 1966

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On a first-order wave theory for a relaxing gas flow

Clarke, J.F. (author)

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

report 1965