Institution
Royal Aircraft Establishment
About: Royal Aircraft Establishment is a based out in . It is known for research contribution in the topics: Geopotential & Satellite. The organization has 1324 authors who have published 1622 publications receiving 43212 citations. The organization is also known as: Royal Aerospace Establishment & Royal Aircraft Factory.
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TL;DR: In this article, it is shown that these features can be obtained by constructing a matrix with a certain property U, i.e., property U is a property of the solution of the Riemann problem.
8,174 citations
01 Oct 1954
TL;DR: In this paper, the optical properties of InSb are analyzed and precise values for the position and temperature dependence of the absorption edge are given, which is explained by the very low effective mass of the conduction electrons, estimated by three methods to be about 0.03 of the free electron mass.
Abstract: The data given on the optical properties of InSb are analysed and precise values for the position and temperature dependence of the absorption edge are given. The variation of the position of the absorption edge with impurity concentration is explained by the very low effective mass of the conduction electrons, which is estimated by three methods to be about 0.03 of the free electron mass.
1,647 citations
01 Nov 1975
TL;DR: In this article, the evolution of the standard is discussed and its application to vehicle ride quality is considered in the context of the safety, efficiency and comfort of crew and passengers, particularly the difficulties of first defining comfort and then postulating appropriate levels.
Abstract: The evolution of the standard, which is aimed at promoting research and production of more data, and providing some design guidance, is outlined and its contents summarized. Some of the assumptions and information on which it is based are analyzed. Its application to vehicle ride quality is considered in the context of the safety, efficiency and comfort of crew and passengers. The importance of establishing the precise criteria against which vibration limits are required is underlined, particularly the difficulties of first defining comfort and then postulating appropriate levels. Some current and future work related to improving the standard is outlined and additional suggestions offered.
626 citations
TL;DR: In this paper, the authors observed the initiation of fatigue cracks at a plane polished surface and the subsequent growth of very short cracks [0.006 mm (0.00025 in.)-0.5 mm(0.02 in.) deep].
496 citations
TL;DR: In this article, a simple triangular finite element for plane elasticity analysis is derived from compatible quadratic displacements with vertex connectors which include rotations, and the results show that quite acceptable accuracy is available for practical applications.
476 citations
Authors
Showing all 1324 results
| Name | H-index | Papers | Citations |
|---|---|---|---|
| Philip L. Roe | 41 | 156 | 17397 |
| John Theodore Houghton | 35 | 104 | 35983 |
| Bruce Chalmers | 32 | 67 | 6620 |
| Malcolm B. Huglin | 32 | 172 | 3474 |
| Michael J. Buckingham | 29 | 134 | 3037 |
| Desmond King-Hele | 27 | 173 | 2639 |
| G. E. Cook | 20 | 43 | 1017 |
| Paul S. Cannon | 19 | 103 | 1301 |
| M. B. Priestley | 18 | 21 | 9160 |
| Andrew Sims | 18 | 107 | 1015 |
| Doreen M.C. Walker | 17 | 75 | 827 |
| D. P. Rooke | 16 | 31 | 2657 |
| Joanne E. Harvey | 15 | 62 | 630 |
| Harbans S. Dhadwal | 14 | 68 | 609 |
| J.K. Lancaster | 13 | 17 | 876 |