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yr

Search results 18

Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-96014] ([NASA contractor report] ; NASA/CR-2001-210849)

Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-96014] ([NASA contractor report] ; NASA/CR-2001-210849)
Microform図書
2001<YCA-NAS 1.26:210849>
National Diet Library
  • Subject Heading...odynamic loads Hypersonic speed Supersonic speed

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny ([NASA technical memorandum] ; NASA/TM-2001-210567)

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny ([NASA technical memorandum] ; NASA/TM-2001-210567)
Microform図書
2001<YCA-NAS 1.15:210567>
National Diet Library
  • Subject HeadingAir breathing boosters Hypersonic speed Computational fluid dynamics ...

Physics of interplanetary dust collection with aerogel [microform] : final report and summary of research : NASA grant NAG-9-913, Johnson Space Center, September 30, 1996-March 31, 1998 / William W. Anderson (NASA/CR ; 1998-207766)

Physics of interplanetary dust collection with aerogel [microform] : final report and summary of research : NASA grant NAG-9-913, Johnson Space Center, September 30, 1996-March 31, 1998 / William W. Anderson (NASA/CR ; 1998-207766)
Microform図書
1998<YCA-NAS 1.26:207766>
National Diet Library
  • Subject HeadingCosmic dust Dust collectors Interplanetary dust Accumulators Hypersonic speed

Multiphysics simulation of active hypersonic lip cooling [microform] / Matthew E. Melis, Wen-Ping Wang (NASA/TM ; 1999-209275)

Multiphysics simulation of active hypersonic lip cooling [microform] / Matthew E. Melis, Wen-Ping Wang (NASA/TM ; 1999-209275)
Microform図書
1999<YCA-NAS 1.15:209275>
National Diet Library
  • Subject HeadingHypersonic speed Computerized simulation Compu...

Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-209015)

Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-209015)
Microform図書
2000<YCA-NAS 1.15:209015>
National Diet Library
  • Subject Heading... Skin friction Hypersonic speed

The NASA Hyper-X Program [microform] / D. Freeman ... [et al.] ([NASA technical memorandum] ; 207243)

The NASA Hyper-X Program [microform] / D. Freeman ... [et al.] ([NASA technical memorandum] ; 207243)
Microform図書
1997<YCA-NAS 1.15:207243>
National Diet Library
  • Subject HeadingTechnologies Hypersonic speed Hypersonic vehicles Data base...

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment [microform] / Leslie Gong and W. Lance Richards (NASA/TM ; 1998-206555)

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment [microform] / Leslie Gong and W. Lance Richards (NASA/TM ; 1998-206555)
Microform図書
1998<YCA-NAS 1.15:206555>
National Diet Library
  • Subject Heading...ermal analysis Hypersonic speed Design analysis

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks (NASA/TP ; 1998-206548)

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks (NASA/TP ; 1998-206548)
Microform図書
1998<YCA-NAS 1.60:206548>
National Diet Library
  • Subject Heading...iles Launching Hypersonic speed Flight tests Airborne equipme...

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF [microform] / H. Douglas Perkins, Scott R. Thomas, and William D. Pack (NASA technical memorandum ; 107384)

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF [microform] / H. Douglas Perkins, Scott R. Thomas, and William D. Pack (NASA technical memorandum ; 107384)
Microform図書
1996<YCA-NAS 1.15:107384>
National Diet Library
  • Subject HeadingIntegral rocket ramjets Engine tests Hypersonic speed Hypersonic wind tunnels

Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements [microform] / W. Lance Richards (NASA technical memorandum ; 4796)

Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements [microform] / W. Lance Richards (NASA technical memorandum ; 4796)
Microform図書
1997<YCA-NAS 1.15:4796>
National Diet Library
  • Subject Heading...yer transition Hypersonic speed Structural design Leading edg...

Effect of fin leading edge sweep on shock-shock interaction at Mach 6 [microform] / Scott A. Berry and Robert J. Nowak (NASA technical memorandum ; 111790)

Effect of fin leading edge sweep on shock-shock interaction at Mach 6 [microform] / Scott A. Berry and Robert J. Nowak (NASA technical memorandum ; 111790)
Microform図書
1996<YCA-NAS 1.15:111790>
National Diet Library
  • Subject HeadingLeading edge sweep Shock wave interaction Wind tunnel tests Hypersonic speed Reynolds number

Vulnerability of Space Station Freedom modules [microform] : a study of the effects of module perforation on crew & equipment : final report ... contract NCC8-28, period 09 September 1993-14 March 1995 / by J. Serrano ... [et al.] ([NASA contractor report] ; NASA-CR-205052)

Vulnerability of Space Station Freedom modules [microform] : a study of the effects of module perforation on crew & equipment : final report ... contract NCC8-28, period 09 September 1993-14 March 1995 / by J. Serrano ... [et al.] ([NASA contractor report] ; NASA-CR-205052)
Microform図書
1995<YCA-NAS 1.26:205031>
National Diet Library
  • Subject Heading... Vulnerability Hypersonic speed Temperature effects

Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis [microform] / Ramadas K. Prabhu (NASA contractor report ; 201606)

Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis [microform] / Ramadas K. Prabhu (NASA contractor report ; 201606)
Microform図書
1996<YCA-NAS 1.26:201606>
National Diet Library
  • Subject Heading... Inviscid flow Hypersonic speed Hypersonic flow Finite elemen...

Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel [microform] / Glen P. Doggett and Ndaona Chokani (NASA contractor report ; 201617)

Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel [microform] / Glen P. Doggett and Ndaona Chokani (NASA contractor report ; 201617)
Microform図書
1996<YCA-NAS 1.26:201617>
National Diet Library
  • Subject Heading...ayer stability Hypersonic speed Navier-Stokes equation Hypers...

Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland (NASA technical paper ; 3476)

Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland (NASA technical paper ; 3476)
Microform図書
1995<YCA-NAS 1.60:3476>
National Diet Library
  • Subject Heading...ersonic inlets Hypersonic speed Inlet flow Internal flow Shoc...

Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne (NASA technical memorandum ; 4756)

Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne (NASA technical memorandum ; 4756)
Microform図書
1997<YCA-NAS 1.15:4756>
National Diet Library
  • Subject HeadingHypersonic vehicles Hypersonic speed Angle of attack Waveriders St...

Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 [microform] / J.E. Bardina, T.J. Coakley ([NASA contractor report] ; NASA-CR-201979)

Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 [microform] / J.E. Bardina, T.J. Coakley ([NASA contractor report] ; NASA-CR-201979)
Microform図書
1994<YCA-NAS 1.26:201979>
National Diet Library
  • Subject Heading...ls Shock waves Hypersonic speed Velocity distribution Boundar...

極超音速ターボジェットエンジンの研究開発

極超音速ターボジェットエンジンの研究開発
Digital文書・図像類
佐藤, 哲也, 田口, 秀之, 下平, 一雄, 小林, 弘明, 岡井, 敬一, 岩瀬, 識, 二村, 尚夫, 森本, 哲也, 小島, 孝之, 藤田, 和央, Sato, Tetsuya, Taguchi, Hideyuki, Shimodaira, Kazuo, Kobayashi, Hiroaki, Okai, Keiichi, Iwase, Shiki, Futamura, Hisao, Morimoto, Tetsuya, Kojima, Takayuki, Fujita, Kazuhisa宇宙航空研究開発機構2004-10-29宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation SystemJAXA-RM-04-009p.21-26
Other Libraries in Japan
  • Subject Heading...洞試験 spaceplane hypersonic speed turbojet engine reusable spac...

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