Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds

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100 1 ‡aBeke, Andrew.
245 1 0 ‡aCriteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds / ‡cAndrew Beke.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c[1956]
300 ‡a17 p. : ‡bill. ; ‡c27 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
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490 0 ‡aNACA research memorandum ; ‡vE55L02A
500 ‡aNACA Research Memorandum E55L02A.
500 ‡a"February 20, 1956."
500 ‡aTitle from cover.
504 ‡aIncludes bibliographical references.
520 3 ‡aAsymmetric air-flow characteristics of supersonic twin-intake air-induction systems were studied with inlets having peak static-pressure recovery at greater than 50-percent mass flow and critical static-pressure recovery equal to or greater than the value at zero mass flow. Analytical predictions of asymmetric flow and initial flow reversal agreed with the experimentally observed trends. Initial flow reversal (i.e., a zero flow in one duct) occurred simultaneously with critical inlet flow in the other duct. Thus, in terms of engine throttling, engine air flow cannot be reduced to less than half the total inlet critical air flow before initial flow reversal occurs.
538 ‡aMode of access: Internet.
650 0 ‡aCharts, diagrams, etc. ‡0http://id.loc.gov/authorities/subjects/sh87002373
650 0 ‡aAerodynamics, Supersonic. ‡0http://id.loc.gov/authorities/subjects/sh85001297
650 0 ‡aAir ducts. ‡0http://id.loc.gov/authorities/subjects/sh85002629
650 0 ‡aAir flow. ‡0http://id.loc.gov/authorities/subjects/sh85002635
650 0 ‡aAirplanes ‡xMotors. ‡0http://id.loc.gov/authorities/subjects/sh85002848
710 2 ‡aLewis Flight Propulsion Laboratory. ‡0http://id.loc.gov/authorities/names/no2015026965 ‡1http://id.loc.gov/rwo/agents/no2015026965 ‡1http://viaf.org/viaf/314909134
710 2 ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics. ‡0http://id.loc.gov/authorities/names/n79060141 ‡1http://id.loc.gov/rwo/agents/n79060141
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
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