Preliminary survey of possible cooling methods for hypersonic aircraft

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040 ‡aFUG ‡cFUG
086 0 ‡aY 3.N 21/5:15/E57L19
099 ‡aNACA RM-E57L19
100 1 ‡aEsgar, Jack B.
245 1 0 ‡aPreliminary survey of possible cooling methods for hypersonic aircraft / ‡cby Jack B. Esgar, Robert O. Hickel, and Francis S. Stepka.
260 ‡aWashington, D.C. : ‡bNACA, ‡c1958.
300 ‡a38 p. : ‡bill. ; ‡c28 cm.
490 0 ‡aNACA RM ‡vE57L19 ‡5FU
500 ‡a"Declassified February 8, 1960." ‡5FU
500 ‡a"Report date January 7, 1958." ‡5FU
504 ‡aIncludes bibliographic references (p. 22-24).
520 3 ‡aAbstract: Many methods of cooling the structure of an aircraft capable of flight speeds up to 18,000 feet per second were studied. Water and hydrogen stored in the liquid state appear very promising as both coolants and heat sinks. The storage and circulation of hydrogen throughout the aircraft need not be a hazard. Cooling the outer skin of the aircraft in high-equilibrium-temperature regions could probably be avoided by using a material such as silicon carbide. The internal structure could be cooled by use of a thin layer of balsa wood saturated with water. In this way tanks for storage of coolant would be avoided.
530 ‡aAlso available in electronic format. ‡5FU
538 ‡aMode of access: Internet.
650 0 ‡aAerodynamics ‡xResearch.
650 0 ‡aAirplanes ‡xMotors ‡xCooling.
650 0 ‡aHypersonic planes.
700 1 ‡aStepka, Francis S.
700 1 ‡aHickel, Robert O.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics.
710 2 ‡aLewis Research Center.
CID ‡a012183198
DAT 0 ‡a20120113135506.0 ‡b20121218000000.0
DAT 1 ‡a20171120114410.0 ‡b2017-11-20T19:57:47Z
DAT 2 ‡a2014-05-22T20:00:04Z
CAT ‡aSDR-UFDC ‡dEX LIBRIS - ALEPH ‡lprepare.pl-004-007
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