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Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility [microform] / Kin C. Wong (NASA/TM-2003-212326)

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility [microform] / Kin C. Wong (NASA/TM-2003-212326)
マイクロ図書
2003<YCA-NAS 1.15:212326>
国立国会図書館
  • 件名...st measurement Exhaust nozzles Nozzle geometry Calibrating

Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector [microform] / Scott C. Asbury ([NASA technical memorandum] ; NASA/TM-97-206255)

Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector [microform] / Scott C. Asbury ([NASA technical memorandum] ; NASA/TM-97-206255)
マイクロ図書
1997<YCA-NAS 1.15:206255>
国立国会図書館
  • 件名Wind tunnel tests Exhaust nozzles Deflectors

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)
マイクロ図書
2000<YCA-NAS 1.55:210524>
国立国会図書館
  • 件名Jet aircraft noise Engine noise Acoustic nozzles Aeroacoustics Sonic nozzles Exhaust nozzles

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control [microform] / Scott C. Asbury and Craig A. Hunter (NASA/TM ; 1999-209513)

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control [microform] / Scott C. Asbury and Craig A. Hunter (NASA/TM ; 1999-209513)
マイクロ図書
1999<YCA-NAS 1.15:209513>
国立国会図書館
  • 件名Exhaust nozzles Porosity Hole geometry (Mecha...

Titanium aluminide applications in the high speed civil transport [microform] / Paul A. Bartolotta and David L. Krause ([NASA technical memorandum] ; NASA/TM-1999-209071)

Titanium aluminide applications in the high speed civil transport [microform] / Paul A. Bartolotta and David L. Krause ([NASA technical memorandum] ; NASA/TM-1999-209071)
マイクロ図書
1999<YCA-NAS 1.15:209071>
国立国会図書館
  • 件名Exhaust nozzles Noise reduction Titanium alum...

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields [microform] / Nicholas J. Georgiadis, Dennis A. Yoder, and James R. DeBonis (NASA/TM ; 1999-209184)

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields [microform] / Nicholas J. Georgiadis, Dennis A. Yoder, and James R. DeBonis (NASA/TM ; 1999-209184)
マイクロ図書
1999<YCA-NAS 1.15:209184>
国立国会図書館
  • 件名Computational grids Ejectors Exhaust nozzles Flow characteristics Navier-S...

Forced mixer nozzle optimization [microform] / Yogi Sheoran ... [et al.] ([NASA contractor report] ; NASA/CR-1999-209160)

Forced mixer nozzle optimization [microform] / Yogi Sheoran ... [et al.] ([NASA contractor report] ; NASA/CR-1999-209160)
マイクロ図書
1999<YCA-NAS 1.26:209160>
国立国会図書館
  • 件名...matics) Mixers Exhaust nozzles Jet engines

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle [microform] / Karen A. Deere and Scott C. Asbury (NASA/TP ; 1999-209138)

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle [microform] / Karen A. Deere and Scott C. Asbury (NASA/TP ; 1999-209138)
マイクロ図書
1999<YCA-NAS 1.60:209138>
国立国会図書館
  • 件名...uation Throats Exhaust nozzles Nozzle design Computational f...

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...s Engine noise Exhaust nozzles Exhaust gases

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam (NASA technical memorandum ; 113181)

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam (NASA technical memorandum ; 113181)
マイクロ図書
1997<YCA-NAS 1.15:113181>
国立国会図書館
  • 件名Exhaust nozzles Nozzle flow Powered lift airc...

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)
マイクロ図書
1994<YCA-NAS 1.60:3411>
国立国会図書館
  • 件名Exhaust nozzles Nozzle geometry Skewness Soni...

ロケット-ラム複合燃焼器の実験

ロケット-ラム複合燃焼器の実験
デジタル規格・テクニカルリポート類
佐藤, 和雄, 坂本, 博, 佐々木, 正樹, 小野, 文衛, 八柳, 信之, Sato, Kazuo, Sakamoto, Hiroshi, Sasaki, Masaki, Ono, Fumiei, Yatsuyanagi, Nobuyuki航空宇宙技術研究所1994-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1249p.1-17
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