D. Shaw

William Temple Foundation

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W. C. Sawyer

Langley Research Center

J. M. Allen

University of Greenwich

E. E. Fletcher

Battelle

J. S. Wilde

Samuel M. Dollyhigh

Analytical Mechanics Associates (United States)

Jackson Kirkman‐Brown

Birmingham Women’s and Children’s NHS Foundation Trust

D. Crockett

Architecture Technology Corporation (United States)

Michael E. Price

Brunel University of London

C. M. Jackson

Langley Research Center

Moataz M. Attallah

University of Birmingham

Cooperative Institutions

Langley Research Center

University of Birmingham

Texas A&M University

Analytical Mechanics Associates (United States)

Birmingham Women’s and Children’s NHS Foundation Trust

Birmingham Women's Hospital

National Health Service

MRC Centre for Reproductive Health

University of Massachusetts Chan Medical School

Architecture Technology Corporation (United States)

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Analysis of selected data from the triservice missile data base

29th Aerospace Sciences Meeting (1989)

J. M. Allen D. Shaw W. C. Sawyer

An extremely large, systematic, axisymmetric-body/tail-fin data base has been gathered through tests of an innovative missile model design which is described herein. These data were originally obtained for incorporation into a missile aerodynamics code based on engineering methods (Program MISSILE3), but these data are also valuable as diagnostic test cases for developing computational methods because of the individual-fin data included in the data base. Detailed analyses of four sample cases from these data are presented to illustrate interesting individual-fin force and moment trends. These samples quantitatively show how bow shock, fin orientation, fin deflection, and body vortices can produce strong, unusual, and computationally challenging effects on individual fin loads. Flow-visualization photographs are examined to provide physical insight into the cause of these effects.

Base (topology)

10.2514/6.1989-478

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Citations (9)

Multiscale Design for the Additive Manufacture of Medical Devices

L.E.J. Thomas-Seale S. Kanagalingam D. Shaw Andrew Triantaphyllou Khamis Essa

Source

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Citations (0)

A transistorized potentiostat system for corrosion studies

Corrosion Science (1965)

D. Shaw A.M. Edwards

Potentiostat

10.1016/0010-938x(65)90001-6

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Citations (10)

Communications on the move

IEE Review (1988)

D. Shaw

Technological advances and more available frequencies are allowing mobile communications to provide an increasing variety of services in an ever more pocket-sized form

10.1049/ir:19880026

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Citations (13)

An automatic potentiostat system for corrosion studies

British Corrosion Journal (1969)

D. Shaw E. E. Fletcher J. S. Wilde

AbstractAbstractManual potentiostatic investigations can be tedious and hence liable to operator errors. An automatic potentlostat system has been designed which requires the minimum of supervision whilst retaining a high degree of control and flexibility. details of experimental results obtained are briefly discussed.

Potentiostat

Operator (biology)

Automatic control

10.1179/bcj.1969.4.5.249

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Citations (1)

William Temple: Fellowship, and Service in Blackburn, Lancashire, and Manchester

Journal of Church and State (2023)

D. Shaw

Journal Article William Temple: Fellowship, and Service in Blackburn, Lancashire, and Manchester Get access David Shaw David Shaw Independent researcher and trustee at the William Temple Foundation E-mail: davyjshaw@googlemail.com https://orcid.org/0000-0001-5941-8602 Search for other works by this author on: Oxford Academic Google Scholar Journal of Church and State, Volume 65, Issue 4, Winter 2023, Pages 385–395, https://doi.org/10.1093/jcs/csad064 Published: 28 November 2023

Temple

10.1093/jcs/csad064

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Citations (0)

Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg

C. D. Babb D. E. Fuller D. Shaw

Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics of blunt bodies

Base (topology)

Cone (formal languages)

Fineness

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Remote control missile model test

J. M. Allen D. Shaw W. C. Sawyer

An extremely large, systematic, axisymmetric body/tail fin data base was gathered through tests of an innovative missile model design which is described herein. These data were originally obtained for incorporation into a missile aerodynamics code based on engineering methods (Program MISSILE3), but can also be used as diagnostic test cases for developing computational methods because of the individual-fin data included in the data base. Detailed analysis of four sample cases from these data are presented to illustrate interesting individual-fin force and moment trends. These samples quantitatively show how bow shock, fin orientation, fin deflection, and body vortices can produce strong, unusual, and computationally challenging effects on individual fin loads. Comparisons between these data and calculations from the SWINT Euler code are also presented.

Fin

Experimental data

Source

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Citations (4)

How the filter press is meeting today's demands

Filtration + Separation (2001)

Michael E. Price D. Shaw

Filtration (mathematics)

Filter press

10.1016/s0015-1882(01)80329-3

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