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Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / / Jeffery A. Yetter, Laurance D. Leavitt
Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / / Jeffery A. Yetter, Laurance D. Leavitt
Autore Yetter Jeffery A.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Descrizione fisica 1 online resource (116 pages) : illustrations
Collana NASA technical paper
Soggetto topico Convergent-divergent nozzles
Exhaust flow simulation
Nozzle design
Static pressure
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707455003321
Yetter Jeffery A.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / / Richard J. Re and Laurence D. Leavitt
Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / / Richard J. Re and Laurence D. Leavitt
Autore Re Richard J.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Descrizione fisica 1 online resource (110 pages) : illustrations
Collana NASA/TP
Soggetto topico Static tests
Thrust vector control
Thrust reversal
Wind tunnel tests
Nozzle geometry
Jet nozzles
Jet planes - Thrust reversers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709716003321
Re Richard J.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / / Bobby L. Berrier and Laurence D. Leavitt
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / / Bobby L. Berrier and Laurence D. Leavitt
Autore Berrier Bobby L.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1984
Descrizione fisica 1 online resource (141 pages) : illustrations
Collana NASA technical paper
Soggetto topico Axisymmetric bodies
Nozzle thrust coefficients
Static tests
Thrust vector control
Transonic wind tunnels
Two dimensional flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees
Record Nr. UNINA-9910707970903321
Berrier Bobby L.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1984
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui