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    <managingEditor>tris-trb@nas.edu (Bill McLeod)</managingEditor>
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      <title>MIT UAV achieves first flights with solid-state propulsion : aircraft skins could produce silent thrust; electroaerodynamic propulsion generates thrust from ionic wind</title>
      <link>https://trid.trb.org/View/1584878</link>
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      <pubDate>Tue, 19 Feb 2019 12:10:25 GMT</pubDate>
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      <title>ENERGY: AN ANNOTATED SELECTED BIBLIOGRAPHY</title>
      <link>https://trid.trb.org/View/170637</link>
      <description><![CDATA[This updated bibliography contains approximately 7,000 selected references on energy and energy related topics from bibliographic and other data sources from June 1977. Under each subject heading the entries are arranged by the date, with the latest works first. Geothermal, solar, wind, and ocean/water power sources are included. Magnetohydrodynamics and electrohydrodynamics, electric power engineering, automotive power plants, and energy storage are also covered.]]></description>
      <pubDate>Tue, 23 Nov 1982 00:00:00 GMT</pubDate>
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      <title>TUNNELING WITH CONTROLLED STRESS WAVES</title>
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      <description><![CDATA[This report describes a concept for hard rock tunneling that uses controlled stress waves to fracture rock. Tests with high explosive charges demonstrated the feasibility of the concept, but follow-on tests with an electrohydraulic stress wave source were unsuccessful. Development of a repeatable stress wave source is necessary to the success of the concept. Extrapolations of test data indicate that the concept could reduce the specific energy requirements for hard rock tunneling by an order of magnitude compared to present tunnel boring machines. (Author)]]></description>
      <pubDate>Wed, 28 Jun 1978 00:00:00 GMT</pubDate>
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      <title>INTERACTION BETWEEN PLANE ELECTROHYDRODYNAMIC JETS</title>
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      <description><![CDATA[Special devices, known as active equalizers, have been developed as one of the methods to control the airplane electrification caused by the loss of charged particles through the engine.  The functioning of these equalizers is based on feeding of charges of the opposite sign to the engine exhaust jet.  It is in this context that the problem of interaction between oppositely charged jets arises.  The need for evaluating interactions between similarly charged jets comes up in designing systems containing multiple equalizers when one must decide on their placement near the exhaust jet.  In the present work, using numerical analysis, the interaction effects of two plane charged jets is studied.  The performance of two electric charge equalizers, as well as equalizers and aircraft engines is modeled.]]></description>
      <pubDate>Wed, 14 Jun 1978 00:00:00 GMT</pubDate>
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