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Issue DateTitleAuthor(s)
Thinking together : new forms of thought system for a revolution in military affairsBurke, M.
1955 Interim Report on Fatigue Characteristics of a Typical Metal WingKepert, J.L.; Payne, A.O.
Feb-1955 Drag of Bare Stranded Cables.Watson, L.T.
1956 Random and Programmed Load Sequence Fatigue Tests on 24ST Aluminium Alloy WingsPayne, A.O.
1956 Fatigue Characteristics of a Riveted 24S-T Aluminium Alloy Wing Part V Discussion of Results and ConclusionsFord, D.G.; Johnstone, W.W.; Kepert, J.L., et al
1956 Fatigue Characteristics of a Riveted 24S-T Aluminium Alloy Wing Part III Test ResultsKepert, J.L.; Patching, C.A.; Rice, M.R., et al
1956 Fatigue Characteristics of a Riveted 24S-T Aluminium Alloy Wing Part II Stress AnalysisRice, M.R.
1959 The Failing Stress of Mustang Wings Weakened by Fatigue CracksPayne, A.O.; Squire, N.L.
Sep-1959 Red Duster Acceptance Trials, scientific evaluation: a mathematical model of the missile system suitable for analogue computationBiggs, A.G.
1960 Application of the Matrix Force Method of Stress Analysis to a Stress Diffusion Problem on the Mustang WingSchmid, L.
Jun-1961 Fatigue Tests on "Mustang" Wings and Notched Aluminium Alloy Specimens Under Random Gust Loading With and Without Ground to Air Cycle of LoadingMann, J.Y.; Patching, C.A.
1962 Fatigue Crack Propagation in Mustang WingsParry-Jones, G.
1964 The Fatigue of 24S-T Aluminium Alloy Wings Under Random Manoeuvre LoadingJost, G.S.
Sep-1964 The Influence of Fretting upon the Fatigue Strength of Materials and Components.Mann, J.Y.
Sep-1964 A circular to rectangular waveguide transition maintaining a constant cutoff wavelengthPYLE, J.R.
Dec-1964 A Comparison of Experimental and Predicted Fatigue Lives of Mustang Wings Under Programmed and Random LoadingJost, G.S.; Lewis, J.A.
Jun-1970 Theoretical assessment of "Demon" performance.d'Assupcao, H.A.
Sep-1972 Computer programmes for the calculation and plotting of the probability of detection of radar targetsRohan, P.
Oct-1972 The estimation of viscous normal force, pitching moment, side force and yawing moment on bodies of revolution at incidences up to 90°.Thompson, K.D.
1973 Anharmonic vibrational relaxation of nitrogen in a nozzleKewley, D.J.
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