Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles /

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Bibliographic Details
Author / Creator:Mason, Mary L., author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, June 1985.
Description:1 online resource (216 pages) : illustrations.
Language:English
Series:NASA/TP ; 2432
NASA technical paper ; 2432.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11618650
Hidden Bibliographic Details
Other authors / contributors:Berrier, Bobby L., author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Langley Research Center.
Notes:"June 1985."
Prepared at Langley Research Center.
Includes bibliographical references (page 19).
Technical paper.
Langley Research Center 505-40-90-01 L-15890
Description based on online resource, PDF version; title from title page (NASA, viewed June 15, 2018).
Other form:Print version: Mason, Mary L Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
Microfiche: Mason, Mary L Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
GPO item no.:0830-H-15 (online)
Govt.docs classification:NAS 1.60:2432

MARC

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264 1 |a Washington, D.C. :  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c June 1985. 
300 |a 1 online resource (216 pages) :  |b illustrations. 
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490 1 |a NASA/TP ;  |v 2432 
500 |a "June 1985." 
500 |a Prepared at Langley Research Center. 
504 |a Includes bibliographical references (page 19). 
513 |a Technical paper. 
536 |a Langley Research Center  |d 505-40-90-01  |d L-15890 
588 |a Description based on online resource, PDF version; title from title page (NASA, viewed June 15, 2018). 
650 7 |a Static tests.  |2 nasat 
650 7 |a Thrust vector control.  |2 nasat 
650 7 |a Convergent-divergent nozzles.  |2 nasat 
650 7 |a Yaw.  |2 nasat 
650 7 |a Wind tunnel tests.  |2 nasat 
650 0 |a Jet nozzles  |x Testing. 
650 0 |a Yawing (Aerodynamics) 
650 0 |a Airplanes  |x Motors  |x Thrust. 
650 7 |a Airplanes  |x Motors  |x Thrust.  |2 fast  |0 (OCoLC)fst00803357 
650 7 |a Jet nozzles  |x Testing.  |2 fast  |0 (OCoLC)fst00982419 
650 7 |a Yawing (Aerodynamics)  |2 fast  |0 (OCoLC)fst01182552 
700 1 |a Berrier, Bobby L.,  |e author.  |0 http://id.loc.gov/authorities/names/n81057962  |1 http://viaf.org/viaf/38237028 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch,  |e issuing body.  |0 http://id.loc.gov/authorities/names/n78091122  |1 http://viaf.org/viaf/269005387 
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776 0 8 |i Microfiche:  |a Mason, Mary L  |t Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles  |w (OCoLC)24762042 
830 0 |a NASA technical paper ;  |v 2432. 
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