LDR | |
02921cam a2200457Ia 4500 |
001 |
|
100167850 |
003 |
|
MiAaHDL |
005 |
|
20250113000000.0 |
006 |
|
m d |
007 |
|
cr bn ---auaua |
008 |
|
110422e195602 dcua tb f000 0 eng d |
035 |
⊔ |
⊔ |
‡a(MiU)990128618060106381
|
035 |
⊔ |
⊔ |
‡asdr-miu.990128618060106381
|
035 |
⊔ |
⊔ |
‡z(MiU)MIU01000000000000012861806-goog
|
035 |
⊔ |
⊔ |
‡a(OCoLC)714160106
|
035 |
⊔ |
⊔ |
‡z(MiU)Aleph012861806
|
040 |
⊔ |
⊔ |
‡aLHL
‡cLHL
‡dNACAR
‡dUtOrBLW
|
049 |
⊔ |
⊔ |
‡aNACA
|
086 |
0 |
⊔ |
‡aY 3.N 21/5:15/E55L02A
|
088 |
⊔ |
⊔ |
‡aNACA RM E55L02A
|
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
|
338 |
⊔ |
⊔ |
‡avolume
‡bnc
‡2rdacarrier
|
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)
|
899 |
⊔ |
⊔ |
‡a39015086463836
|
CID |
⊔ |
⊔ |
‡a100167850
|
DAT |
0 |
⊔ |
‡a20241218082754.0
‡b20250113000000.0
|
DAT |
1 |
⊔ |
‡a20250113232106.0
‡b2025-01-14T16:46:22Z
|
DAT |
2 |
⊔ |
‡a2024-03-16T17:30:02Z
|
CAT |
⊔ |
⊔ |
‡aSDR-MIU
‡cmiu
‡dALMA
‡lprepare.pl-004-009
|
FMT |
⊔ |
⊔ |
‡aBK
|
HOL |
⊔ |
⊔ |
‡0sdr-miu.990128618060106381
‡aMiU
‡bSDR
‡cGWLA
‡f012861806
‡pmdp.39015086463836
‡sMIU
‡1990128618060106381
|
974 |
⊔ |
⊔ |
‡bMIU
‡cGWLA
‡d20250114
‡sgoogle
‡umdp.39015086463836
‡y1956
‡rpd
‡qbib
‡tUS fed doc
|