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02138nam a2200493Ia 4500 |
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c7be4f76-4a02-4fa4-baeb-cb89bed42bfe |
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20230617000000.0 |
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060908s1970 dcua bt f000 0 eng d |
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|a 19700015497
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8 |
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|a 70N24802
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024 |
8 |
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|a N7024802
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035 |
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|a (OCoLC-I)660646292
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|a (OCoLC-M)71274622
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040 |
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|a FER
|c FER
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088 |
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|a E-5459
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100 |
1 |
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|a Burley, Richard R
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245 |
1 |
0 |
|a Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generator /
|c by Richard R. Burley and Ali H. Mansour
|
260 |
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|a Washington, D.C. :
|b National Aeronautics and Space Administration ;
|a Springfield, Va. :
|b For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor],
|c 1970
|
300 |
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|a 46 p. :
|b ill. ;
|c 27 cm
|
490 |
1 |
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|a NASA technical memorandum ;
|v X-1999
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500 |
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|a Cover title
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500 |
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|a Performing organization report no.: E-5459
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500 |
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|a "April 1970."
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500 |
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|a "NASA TM X-1999."
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504 |
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|a Includes bibliographical references (p. 15)
|
536 |
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|a Performed by Lewis Research Center, Cleveland, Ohio
|h 720-03
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596 |
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|a 31
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650 |
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7 |
|a Afterburning
|2 nasat
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650 |
|
7 |
|a Exhaust nozzles
|2 nasat
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650 |
|
7 |
|a Gas generators
|2 nasat
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650 |
|
7 |
|a Graphs (charts)
|2 nasat
|
650 |
|
7 |
|a Nozzle design
|2 nasat
|
650 |
|
7 |
|a Nozzle efficiency
|2 nasat
|
650 |
|
7 |
|a Pressure gradients
|2 nasat
|
650 |
|
7 |
|a Propulsion system performance
|2 nasat
|
650 |
|
7 |
|a Supersonic flight
|2 nasat
|
650 |
|
7 |
|a Takeoff
|2 nasat
|
650 |
|
7 |
|a Temperature profiles
|2 nasat
|
650 |
|
7 |
|a Transonic flight
|2 nasat
|
700 |
1 |
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|a Mansour, Ali H
|? UNAUTHORIZED
|
710 |
2 |
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|a Lewis Research Center
|
830 |
|
0 |
|a NASA technical memorandum
|v X-1999
|
999 |
1 |
0 |
|i c7be4f76-4a02-4fa4-baeb-cb89bed42bfe
|l a8638032
|s US-CST
|m static_performance_of_an_auxiliary_inlet_ejector_nozzle_using_an_after_____1970_______natioa________________________________________burley__richard_r__________________p
|
999 |
1 |
1 |
|l a8638032
|s ISIL:US-CST
|t BKS
|a SAL3 STACKS
|b 36105024774460
|c NASA TM X-1999
|d ALPHANUM
|x STKS-MONO
|y 36105024774460
|p LOANABLE
|