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Near field trailing edge tone noise computation [microform] / Ching Y. Loh ; [prepared for the 41st Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-9, 2003 ; prepared under contract NAS3-97186] AIAA-2003-0365 (NASA/CR-2002-212013)

Near field trailing edge tone noise computation [microform] / Ching Y. Loh ; [prepared for the 41st Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-9, 2003 ; prepared under contract NAS3-97186] AIAA-2003-0365 (NASA/CR-2002-212013)
Microform図書
2002<YCA-NAS 1.15:2002-212013>
National Diet Library
  • Subject HeadingComputation Aeroacoustics Aerodynamic noise Blunt trailing edges Flow noise Near fields

Heat transfer in a complex trailing edge passage for a high pressure turbine blade. Pt. 2, Simulation results [microform] / David L. Rigby, Ronald S. Bunker 2002-GT-30213 (NASA/CR-2002-211701)

Heat transfer in a complex trailing edge passage for a high pressure turbine blade. Pt. 2, Simulation results [microform] / David L. Rigby, Ronald S. Bunker 2002-GT-30213 (NASA/CR-2002-211701)
Microform図書
2002<YCA-NAS 1.15:2002-211701>
National Diet Library
  • Subject HeadingTrailing edges Turbine blades Computerized s...

Predicting modes of the unsteady vorticity field near the trailing edge of a blade [microform] / William J. Devenport and Nicolas Spitz (NASA/CR-2003-212099)

Predicting modes of the unsteady vorticity field near the trailing edge of a blade [microform] / William J. Devenport and Nicolas Spitz (NASA/CR-2003-212099)
Microform図書
2003<YCA-NAS 1.26:212099>
National Diet Library
  • Subject HeadingVorticity Aerodynamic noise Trailing edges Noise prediction (Aircraft) T...

Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program [microform] / Bruce Charles ([NASA contractor report] ; NASA/CR-1999-209327)

Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program [microform] / Bruce Charles ([NASA contractor report] ; NASA/CR-1999-209327)
Microform図書
1999<YCA-NAS 1.26:209327>
National Diet Library

Optimum transonic airfoils based on the Euler equations [microform] / Angelo Iollo, Manuel D. Salas

Optimum transonic airfoils based on the Euler equations [microform] / Angelo Iollo, Manuel D. Salas
Microform図書
1997<YCA-NAS 1.26:201638>
National Diet Library
  • Subject HeadingTransonic flight Transonic flow Airfoils Euler equations of motion Trailing edges

High-lift systems on commercial subsonic airliners [microform] / Peter K.C. Rudolph (NASA contractor report ; 4746)

High-lift systems on commercial subsonic airliners [microform] / Peter K.C. Rudolph (NASA contractor report ; 4746)
Microform図書
1996<YCA-NAS 1.26:4746>
National Diet Library
  • Subject Heading...ing edge flaps Trailing edges Wing loading Wing camber Wing...

An experimental investigation of the confluent boundary layer on a high-lift system [microform] : final project report / by F.O. Thomas and R.C. Nelson

An experimental investigation of the confluent boundary layer on a high-lift system [microform] : final project report / by F.O. Thomas and R.C. Nelson
Microform図書
1997<YCA-NAS 1.26:112979>
National Diet Library
  • Subject Heading...boundary layer Trailing edges Vortex flaps Flow characteris...

Application of particle image velocimetry to a study of flow about a multi-element airfoil [microform] : final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155 / by the Department of Aeronautics and Astronautics, Stanford University ; Stephen M. Walker; Donald Baganoff, principal investigator ([NASA contractor report] ; NASA-CR-202724)

Application of particle image velocimetry to a study of flow about a multi-element airfoil [microform] : final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155 / by the Department of Aeronautics and Astronautics, Stanford University ; Stephen M. Walker; Donald Baganoff, principal investigator ([NASA contractor report] ; NASA-CR-202724)
Microform図書
1996<YCA-NAS 1.26:202724>
National Diet Library

Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap [microform] / Ahmed Hassan ([NASA contractor report] ; NASA/CR-1999-209328)

Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap [microform] / Ahmed Hassan ([NASA contractor report] ; NASA/CR-1999-209328)
Microform図書
1999<YCA-NAS 1.26:209328>
National Diet Library

Active spanwise lift control : a distributed parameter approach

Active spanwise lift control : a distributed parameter approach
Paper図書
Joaquim Neto Dias, James E. Hubbard, Jr.American Institute of Aeronautics and Astronauticsc2020
Other Libraries in Japan

Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck (NASA technical paper ; 3579)

Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck (NASA technical paper ; 3579)
Microform図書
1996<YCA-NAS 1.60:3579>
National Diet Library
  • Subject Heading...eynolds number Trailing edges Transonic wind tunnels Aerody...

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall (NASA technical paper ; 3516)

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall (NASA technical paper ; 3516)
Microform図書
1995<YCA-NAS 1.60:3516>
National Diet Library
  • Subject Heading...Subsonic speed Trailing edges Transonic speed Wind tunnel t...

Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury (NASA technical paper ; 3440)

Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury (NASA technical paper ; 3440)
Microform図書
1994<YCA-NAS 1.60:3440>
National Diet Library
  • Subject Heading...eometry Thrust Trailing edges Transonic speed Wind tunnel t...

超音速流中におけるダイヤモンド翼の剥離制御

超音速流中におけるダイヤモンド翼の剥離制御
Digital文書・図像類
新井, 隆景, 坂上, 昇史, Arai, Takakage, Sakaue, Shoji宇宙航空研究開発機構2007-09-03宇宙航空研究開発機構契約報告: サイレント超音速機に関する調査研究:平成18年(2006年)度研究成果報告書 = JAXA Contract Report: Survey and Research on Silent Supersonic Aircraft: Report on the Research Results of FY2006JAXA-CR-07-001p.43-73
Other Libraries in Japan

ワークショップ翼型失速特性シミュレーション.結果のまとめ:CFDは翼型失速角を予測できるか?

ワークショップ翼型失速特性シミュレーション.結果のまとめ:CFDは翼型失速角を予測できるか?
Digital文書・図像類
廣瀬, 直喜, 中橋, 和博, 吉田, 憲司, 松尾, 裕一, 岩宮, 敏幸, Hirose, Naoki, Nakahashi, Kazuhiro, Yoshida, Kenji, Matsuo, Yuichi, Iwamiya, Toshiyuki航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.175-177
Other Libraries in Japan

ワークショップ翼型失速特性シミュレーション2DST-6:CFDは翼型失速角を予測できるか

ワークショップ翼型失速特性シミュレーション2DST-6:CFDは翼型失速角を予測できるか
Digital文書・図像類
松島, 紀佐, 岩宮, 敏幸, Matsushima, Kisa, Iwamiya, Toshiyuki航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.147-150
Other Libraries in Japan

Flap deflection optimization for transonic cruise performance improvement of supersonic transport wing

Flap deflection optimization for transonic cruise performance improvement of supersonic transport wing
Digital文書・図像類
Kim, Hyoung-Jin, 大林, 茂, 中橋, 和博, Obayashi, Shigeru, Nakahashi, Kazuhiro航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.267-274
Other Libraries in Japan
  • Note (General)...s and five for trailing edges, are employed as design varia...

Prediction of airfoil stall by using Launder-Sharma turbulence model

Prediction of airfoil stall by using Launder-Sharma turbulence model
Digital文書・図像類
Lei, Zhong, 岩宮, 敏幸, Iwamiya, Toshiyuki航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.157-162
Other Libraries in Japan

CFDは翼型失速角を予測できるか?:乱流モデルの比較

CFDは翼型失速角を予測できるか?:乱流モデルの比較
Digital文書・図像類
松本, 崇, Matsumoto, Takashi航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.123-128
Other Libraries in Japan

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