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Search results 4

AST critical propulsion and noise reduction technologies for future commercial subsonic engines [microform] : separate-flow exhaust system noise reduction concept evaluation / B.A. Janardan ... [et al.] ([NASA contractor report] ; NASA/CR-2000-210039)

AST critical propulsion and noise reduction technologies for future commercial subsonic engines [microform] : separate-flow exhaust system noise reduction concept evaluation / B.A. Janardan ... [et al.] ([NASA contractor report] ; NASA/CR-2000-210039)
Microform図書
2000<YCA-NAS 1.26:210039>
National Diet Library
  • Subject HeadingAcoustic nozzles Aeroacoustics Engine noise Jet aircraft noise Noise reduction Sonic nozzles

Separate flow nozzle test status meeting [microform] : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 / [Naseem H. Saiyed, editor] ([NASA conference publication] ; NASA/CP-2000-210524)

Separate flow nozzle test status meeting [microform] : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 / [Naseem H. Saiyed, editor] ([NASA conference publication] ; NASA/CP-2000-210524)
Microform図書
2000<YCA-NAS 1.55:210524>
National Diet Library
  • Subject HeadingJet aircraft noise Engine noise Acoustic nozzles Aeroacoustics Sonic nozzles Exhaust nozzles

Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle [microform] / Michael K. Ponton, John M. Seiner, and Martha C. Brown (NASA technical memorandum ; 113137)

Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle [microform] / Michael K. Ponton, John M. Seiner, and Martha C. Brown (NASA technical memorandum ; 113137)
Microform図書
1997<YCA-NAS 1.15:113137>
National Diet Library
  • Subject HeadingSonic nozzles Transonic nozzles Supersonic nozzles Pressure oscillations Flame p...

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept [microform] / David J. Wing (NASA technical paper ; 3411)

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept [microform] / David J. Wing (NASA technical paper ; 3411)
Microform図書
1994<YCA-NAS 1.60:3411>
National Diet Library
  • Subject Heading...metry Skewness Sonic nozzles Static tests Throats Thrust v...

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