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Journal Articles

Safe Access for Maintenance — Aero‐Docks Technique

D. Williams, I.R. Bristow

Aircraft Engineering (1975) 47 (8): 15–18.

https://doi.org/10.1108/eb035267

Published: 01 August 1975

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Journal Articles

Developments in the Structural Approach to Aero‐Elastic Problems: The Spoken Version of the Lecture Read before the Royal Aeronautical Society on February 11, 1954, and Published with Full Mathematical Development in the Journal for June 1954

D. Williams, D.Sc., M.I.Mech.E., F.R.Ae.S.

Aircraft Engineering (1954) 26 (9): 303–307.

https://doi.org/10.1108/eb032471

Published: 01 September 1954

View article titled, Developments in the Structural Approach to Aero‐Elastic Problems: The Spoken Version of the Lecture Read before the Royal Aeronautical Society on February 11, 1954, and Published with Full Mathematical Development in the Journal for June 1954

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Journal Articles

The Library Shelf

D. WILLIAMS, W.J. DUNCAN

Aircraft Engineering (1947) 19 (12): 388–389.

https://doi.org/10.1108/eb031582

Published: 01 December 1947

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Journal Articles

Two Books Received From America

D. WILLIAMS, IVOR LUSTY

Aircraft Engineering (1945) 17 (6): 177–178.

https://doi.org/10.1108/eb031256

Published: 01 June 1945

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Journal Articles

Models in Structural Research: An Aid to the Designer in Solving Difficult Problems in Stressed‐Skin Structures

D. Williams, D.Sc., A.M.I.Mech.E.

Aircraft Engineering (1939) 11 (6): 231–232.

https://doi.org/10.1108/eb030496

Published: 01 June 1939

View article titled, Models in Structural Research: An Aid to the Designer in Solving Difficult Problems in Stressed‐Skin Structures

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Journal Articles

Openings in Stressed‐Skin Wings: The Effect of Cover Discontinuities on the Strength and Stiffness of Stressed‐Skin Wings

D. Williams, B.Sc., A.M.I.Mech.E.

Aircraft Engineering (1938) 10 (1): 3–6.

https://doi.org/10.1108/eb030260

Published: 01 January 1938

View article titled, Openings in Stressed‐Skin Wings: The Effect of Cover Discontinuities on the Strength and Stiffness of Stressed‐Skin Wings

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Journal Articles

Critical Loads of Long Struts: The Case of a Strut with Elastic End Constraints of Finite Amount

D. Williams, B.Sc., A.M.I.Mech.E.

Aircraft Engineering (1933) 5 (12): 297–298.

https://doi.org/10.1108/eb029753

Published: 01 December 1933

View article titled, Critical Loads of Long Struts: The Case of a Strut with Elastic End Constraints of Finite Amount

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Safe Access for Maintenance — Aero‐Docks Technique

Developments in the Structural Approach to Aero‐Elastic Problems: The Spoken Version of the Lecture Read before the Royal Aeronautical Society on February 11, 1954, and Published with Full Mathematical Development in the Journal for June 1954

The Library Shelf

Two Books Received From America

Models in Structural Research: An Aid to the Designer in Solving Difficult Problems in Stressed‐Skin Structures

Openings in Stressed‐Skin Wings: The Effect of Cover Discontinuities on the Strength and Stiffness of Stressed‐Skin Wings

Critical Loads of Long Struts: The Case of a Strut with Elastic End Constraints of Finite Amount

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