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Oosting, M. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Faasen, N.J. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Klinkenberg, J.W. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Litan, R.E. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Vermeulen, C.G. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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De Graaff, J. (author), Eigeman, J. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Kirkby, S. (author), Nonweiler, T. (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 1953
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Howe, D. (author)The root constraint problem associated with iiniform rectangular swept boxes, having ribs normal to the spars is considered. A strain energy method using self-equilibrating internal end load systems is used. Solutions are presented for the cases of a single cell box having either all ribs rigid, or the root rib flexible. In addition, a...report 1953
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Howe, D. (author)This report is concerned with the application of various theories to the solution of problems investigated experimentally, and in some cases theoretically, by others at the College of Aeronautics. The following work is considered: -A single cell swept wing with ribs normal to the spars, a strain energy solution, allowing for a flexible root rib...report 1953
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Stijntjes, G.J.F. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Bruyn, J. (author), Houwink, E.H. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Madlener, C.F. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Gottschal, A.J. (author), Kooy, C.L.D. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Young, A.D. (author)The effects of viscosity on the aerodynamic characteristics of wings and bodies at supersonic speeds can be assessed if we can calculate (a) the development of the boundary layers in the laminar and turbulent states, (b) the interaction of the boundary layers and main stream away from the neighbourhood of shock waves, (c) the effects of shock...report 1953
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Langley, R.A. (author), Bethwaite, C.F. (author)The problems of detecting and indicating an approaching stall have been investigated in flight on an "Anson" aircraft. A lower-surface flap near the leading-edge of the wing detects the approaching stall at a speed which depends critically on the length of the flap and on its location, but the margin of warning speed over stalling-speed is...report 1953
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Brugman, A.H.M. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Tien, L.T. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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Van Laar, G. (author)Document(en) uit de collectie Chemische Procestechnologiereport 1953
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- Muskens, G.J.A.M. (author) report 1953