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Journal Articles

Quantitative methods of predicting relative effectiveness of corrosion inhibitive coatings

K.J. Lewis, J.H. Aklian, A. Sharaby, J.D. Zook
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology: An International Journal (1996) 68 (3): 12–22.
https://doi.org/10.1108/eb037634
Published: 01 March 1996
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Journal Articles

Advanced Digital Avionics of the DC‐9 Super 80

J.H. ARMSTRONG, J.D. McDONNELL
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1980) 52 (5): 13–18.
https://doi.org/10.1108/eb035626
Published: 01 May 1980
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Journal Articles

Canopy development for the Cranfield A1

J.H. Webb
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1977) 49 (6): 6–8.
https://doi.org/10.1108/eb035391
Published: 01 June 1977
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Journal Articles

Head‐up and other Displays

J.H. Smith, R.A. Chorley
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1975) 47 (2): 18–22.
https://doi.org/10.1108/eb035226
Published: 01 February 1975
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Journal Articles

Past, Present and Future: Comment from former distinguished contributors

J.H. Argyris, D.Sc.(Eng.), D.E., Hon. A.C.G.I., F.R.Ae.S., Air Cdre. F.R. Banks, C.B., O.B.E., Hon. F.A.I.A.A., Hon. F.R.Ae.S., F.I.Mech.E., F.Inst.P., A.D. Baxter, M.Eng., C.Eng., M.I.Mech.E., F.R.Ae.S., F.Inst.Pat.
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1970) 42 (10): 6–7.
https://doi.org/10.1108/eb034682
Published: 01 October 1970
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Journal Articles

Aerodynamic Design Features of the C‐5A: An account of some of the problems encountered and the solutions adopted in the design of the Galaxy

J.H. Paterson
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1968) 40 (6): 8–15.
https://doi.org/10.1108/eb034383
Published: 01 June 1968
View article titled, Aerodynamic Design Features of the C‐5A: An account of some of the problems encountered and the solutions adopted in the design of the Galaxy
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Journal Articles

Inspection of Non‐Metallic Materials

J.H. Joyce
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1967) 39 (12): 19–21.
https://doi.org/10.1108/eb034320
Published: 01 December 1967
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Journal Articles

Aircraft Systems

J.H. Renshaw, D.C.Ae.
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1965) 37 (3): 93–99.
https://doi.org/10.1108/eb033999
Published: 01 March 1965
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Journal Articles

Comparative Performance of Five Chipmunk Aircraft: An Investigation of the Assumption that the Performance of any Operational Aircraft can be considered to be Representative of that Type of Aircraft

J.H. Fawcett, B.Sc.(Eng.)
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1964) 36 (5): 140–145.
https://doi.org/10.1108/eb033872
Published: 01 May 1964
View article titled, Comparative Performance of Five Chipmunk Aircraft: An Investigation of the Assumption that the Performance of any Operational Aircraft can be considered to be Representative of that Type of Aircraft
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1961) 33 (8): 227–238.
https://doi.org/10.1108/eb033442
Published: 01 August 1961
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1961) 33 (7): 193–200.
https://doi.org/10.1108/eb033431
Published: 01 July 1961
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1961) 33 (6): 164–174.
https://doi.org/10.1108/eb033420
Published: 01 June 1961
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1961) 33 (4): 103–113.
https://doi.org/10.1108/eb033398
Published: 01 April 1961
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1961) 33 (3): 71–83.
https://doi.org/10.1108/eb033386
Published: 01 March 1961
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1961) 33 (2): 34–45.
https://doi.org/10.1108/eb033371
Published: 01 February 1961
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1959) 31 (9): 272–283.
https://doi.org/10.1108/eb033156
Published: 01 September 1959
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1959) 31 (8): 244–256.
https://doi.org/10.1108/eb033148
Published: 01 August 1959
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1959) 31 (7): 192–203.
https://doi.org/10.1108/eb033133
Published: 01 July 1959
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1959) 31 (6): 169–179.
https://doi.org/10.1108/eb033125
Published: 01 June 1959
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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Journal Articles

The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer

J.H. Argyris, S. Kelsey
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1959) 31 (5): 133–143.
https://doi.org/10.1108/eb033113
Published: 01 May 1959
View article titled, The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
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