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Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing ([NASA technical paper] ; NASA/TP-1998-206912)

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing ([NASA technical paper] ; NASA/TP-1998-206912)
マイクロ図書
1998<YCA-NAS 1.60:206912>
国立国会図書館
  • 件名...ozzle geometry Convergent nozzles Angular distribution Flow dis...

Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet [microform] / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee (NASA/TM ; 1999-209336)

Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet [microform] / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee (NASA/TM ; 1999-209336)
マイクロ図書
1999<YCA-NAS 1.15:209336>
国立国会図書館
  • 件名Aeroacoustics Convergent nozzles Jet flow Subsonic flow High R...

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters [microform] / E. Ann Bare and Francis J. Capone (NASA technical memorandum ; 4112)

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters [microform] / E. Ann Bare and Francis J. Capone (NASA technical memorandum ; 4112)
マイクロ図書
1989<YCA-NAS 1.15:4112>
国立国会図書館
  • 件名Jet nozzles -- Testing Convergent nozzles Nozzle design Nozzle geometry...

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