Results 251 to 260 of about 24,416 (308)
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Aircraft Engineering and Aerospace Technology, 1944
DURING 1943, we published two papers, both from foreign sources, on electric gauges to measure the strains in aeroplane structures. The second of these, which logically should have come first, appeared in our April issue and was an MAP. translation from the German which covered the theory of electric resistance strip and ring gauges.
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DURING 1943, we published two papers, both from foreign sources, on electric gauges to measure the strains in aeroplane structures. The second of these, which logically should have come first, appeared in our April issue and was an MAP. translation from the German which covered the theory of electric resistance strip and ring gauges.
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Titanium and Aircraft Engineering
Aircraft Engineering and Aerospace Technology, 1959TITANIUM, with a melting point of 1,660 deg. C, higher than that of nickel or iron, a density little more than one‐half that of steel, and a corrosion resistance in certain environments superior to stainless steel, is evidently a metal of significance to aeronautics.
A.J. Kennedy, A.R. Sollars
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Magnesium and Aircraft Engineering
Aircraft Engineering and Aerospace Technology, 1960MAGNESIUM, because of its low density, has obvious possibilities as an aircraft structural material. The useful magnesium alloys have densities in the range 1·76 to 1·83, compared with the aluminium alloys range of about 2·5 to 2·8. The melting point of magnesium is 650 deg. C., almost identical with that of aluminium (660 deg.
A.J. Kennedy, A.R. Sollars
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Aerodynamic aspects of engine-aircraft integration of transport aircraft
Aerospace Science and Technology, 1997The contribution highlights different aspects of engine-airframe integration and summarizes areas of concern for engine installation such as, engine development trends, turbofan integration with respect to advanced engine concepts, programmes and investigations on propeller integration, application of theoretical methods in particular with respect to ...
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Aluminium and Aircraft Engineering
Aircraft Engineering and Aerospace Technology, 1960ALUMINIUM alloys have been important structural materials in aircraft from very early days, and there is no doubt that the course of aeronautical development would have been very different without them. It would be pointless to review the classification of these alloys and their respective fields of application in quite the same way as was done in the ...
A.J. Kennedy, A.R. Sollars
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Computing machines in aircraft engineering
Papers and discussions presented at the Dec. 10-12, 1951, joint AIEE-IRE computer conference: Review of electronic digital computers on - AIEE-IRE '51, 1951A critical evaluation of computing machinery is given from the viewpoint of the aeronautical engineer. The machines' limitations are presented together with suggestions to make them more useful in the aircraft industry.
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SAE Technical Paper Series, 1930
<div class="htmlview paragraph"><b>T</b>HE PAPER urges united cooperation instead of the present division of responsibility between the engine designer and the airplane designer in the installation of aircraft engines. The tubular rings upon which engines are commonly mounted are usually supported by structural members that are welded
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<div class="htmlview paragraph"><b>T</b>HE PAPER urges united cooperation instead of the present division of responsibility between the engine designer and the airplane designer in the installation of aircraft engines. The tubular rings upon which engines are commonly mounted are usually supported by structural members that are welded
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Aircraft-Engine-Accessory Vibration
Transactions of the American Institute of Electrical Engineers, 19441. The overhang-moment limit, or still better a limit on the moment of inertia of the accessory about a line through the center of the accessory mounting surface, would be helpful by limiting one of the two factors which control the natural frequency of the accessory-rear-cover combination.
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Aircraft Engines and the Future
Aircraft Engineering and Aerospace Technology, 1930THE Wilbur Wright Lecture this year is certainly one of the most thought‐provoking that has been delivered. Read in conjunction with the James Forrest Lecture, printed in our last issue, it gives a very complete picture of where we stand in aircraft and engines to‐day. This general survey comes very appropriately in time to appear in this number, which
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Aircraft Engineering in Singapore
Aircraft Engineering and Aerospace Technology, 1978There are times when the present state of an organisation cannot be fully appreciated without reference to the past. This is certainly true of Singapore International Airlines.
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