Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generator /

Bibliographic Details
Main Author: Burley, Richard R
Corporate Author: Lewis Research Center
Other Authors: Mansour, Ali H
Format: Book
Language:English
Published: Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970
Series:NASA technical memorandum X-1999
Subjects:
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008 060908s1970 dcua bt f000 0 eng d
024 8 |a 19700015497 
024 8 |a 70N24802 
024 8 |a N7024802 
035 |a (OCoLC-I)660646292 
035 |a (OCoLC-M)71274622 
040 |a FER  |c FER 
088 |a E-5459 
100 1 |a Burley, Richard R 
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 |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 |a 46 p. :  |b ill. ;  |c 27 cm 
490 1 |a NASA technical memorandum ;  |v X-1999 
500 |a Cover title 
500 |a Performing organization report no.: E-5459 
500 |a "April 1970." 
500 |a "NASA TM X-1999." 
504 |a Includes bibliographical references (p. 15) 
536 |a Performed by Lewis Research Center, Cleveland, Ohio  |h 720-03 
596 |a 31 
650 7 |a Afterburning  |2 nasat 
650 7 |a Exhaust nozzles  |2 nasat 
650 7 |a Gas generators  |2 nasat 
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 |a Mansour, Ali H  |? UNAUTHORIZED 
710 2 |a Lewis Research Center 
830 0 |a NASA technical memorandum  |v X-1999 
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