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Nonweiler, T. (author)The stability derivatives of a delta wing of small aspect ratio, mounted on a cylindrical body with a slender pointed head, are derived by considering the flow in planes perpendicular to the body axis to be uninfluenced by the change in the streamwise component of the air velocity (the so-called 'slender body' theory). The results are tabulated,...report 1951
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Laurmann, J.A. (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 1951
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- Anderson, J.R. (author), Treadgold, D. (author) report 1951
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Ripley, E.L. (author)A method is presented by which structure weight can be predicted from data available in the early project stage of a new design. An important feature of the method is that parts having distinct structural functions are treated separately. The formulae and graphs are derived from a theoretical analysis and are then adjusted empirically to...report 1951
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Lord, W.T. (author), Beastall, D. (author)This note presents a method of finding the errors to be expected in deriving the Mach number at a point in a supersonic flow from the three formulae which depend on the pitot , static and stagnation pressures at that point, when the errors involved in the pressure readings can be estimated . It thus suggests the best formula to use in any given...report 1951
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Lewis, S.R. (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 1951
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Heald, W.R. (author)A thin stiffened metal cylinder liable to General Instability was tested under axial compression and an investigation was made into possible methods of predicting the critical load from non-destructive tests. Particular attention was paid to the perturbation loading technique. The cylinder was finally tested to destruction and the actual failing...report 1951
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Radok, J.R.M. (author)The equations of motion of a uniform swept box with stringers and ribs are deduced. For the case of vibrations of a cantilever they are transformed into integral equations, an approximate method of solution of which is indicated. The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield...report 1951
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Babister, A.W. (author), Lilley, G.M. (author), Sills, E.C. (author), Deards, S.R. (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 1951
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Babister, A.W. (author)Summary of wind tunnel work at the College of Aeronautics 1948 - 50. 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 1951
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- report 1950
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- Patterson, G.N. (author) report 1950
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Ripley, E.L. (author)This report presents a simple and accurate method of predicting fuselage structure weight from data available in the early project stage of a new design. The method was evolved by analysis of fuselage structure weights for over sixty aircraft. It requires a knowledge of the general layout of the fuselage, the external dimensions and the design...report 1950
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Robinson, A. (author)A method is developed for the calculation of the aerodynamic forces acting on a 'swallow tail' wing of small aspect ratio. Lift, induced drag, and aerodynamic centre position of simple swallow tail wings (Fig.1(b)) are computed as an application. For a given incidence, lift and induced drag are, within the limits of the theory, proportional to...report 1950
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Buchan, A.L. (author), Harris, K.D. (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 1950
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Babister, A.W. (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 1950
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Burt, M.E. (author), Ripley, E.L. (author)This report presents a simple but accurate method of predicting undercarriage weight from data which would be available in the early project stage of a new design. The method was evolved by analysis of the weights of main components of undercarriages for over fifty aircraft types and tracing the features which influence undercarriage weight.report 1950
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Bolton Shaw, B.W. (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 1950
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Robinson, A. (author)The field of flow due to a shock wave or expansion wave undergoes a considerable modification in the neighbourhood of a rigid wall. It has been suggested that the resulting propagation of the disturbance upstream is largely due to the fact that the main flow in the boundary layer is subsonic. Simple models were produced by Howarth, and Tsien and...report 1950
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Young, A.D. (author), Booth, T.B. (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 1950