Výsledky vyhledávání - "wing nacelle interference"

Dissertation/ Thesis

Análise experimental e teórica do efeito de uma Nacele \'Pusher\' nas características aerodinâmicas de um avião bimotor

Autor: Palota, Paulo Henrique

Esse trabalho descreve uma investigação prática e teórica de características aerodinâmicas de um modelo referente a um avião bimotor leve \"Piper PA-34 SENECA III\" construído em escala 1:6,5. Basicamente, duas configurações fazem parte da

Externí odkaz: http://www.teses.usp.br/teses/disponiveis/18/18135/tde-17022016-123236/

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CFD based design system for engine nacelle integration on HSCT

Autor: Kano, Shintaro, Nakahashi, Kazuhiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 37:75-80

航空宇宙技術研究所 12-13 Jun. 1997 東京日本
National Aerospace Laboratory 12-13 Jun. 1997 Tokyo Japan
超音速旅客機(HSCT)におけるエンジンナセル統合化のためのCFD(数値流体力学)による設計シス�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0645d7f6a634acf453e44033248a40cc
http://id.nii.ac.jp/1696/00037132/

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Numerical analysis about the wing-nacelle interference of supersonic transport

Autor: Yamazaki, Tetsuo, Uchida, Takashi

Publikováno v: 航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集 = Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics. 22:225-229

航空宇宙技術研究所 10-11 Jun. 1993 東京日本
National Aerospace Laboratory 10-11 Jun. 1993 Tokyo Japan
超音速輸送機では、一般にエンジンは主翼の下に取り付けられる。この場合、主翼の翼厚や�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2ca42f1c263e4f495137189ff6096669
http://id.nii.ac.jp/1696/00037793/

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Numerical analysis on wing/nacelle interference using overlapped grid method

Autor: Tani, Yasuhiro, Amano, Kanichi

航空宇宙技術研究所 10-11 Jun. 1993 東京日本
National Aerospace Laboratory 10-11 Jun. 1993 Tokyo Japan
輸送機形態に関する主翼/ナセル干渉の数値解析を行った。干渉抵抗を減らすためのリプレッ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4a764608cb2d4188411d6b4e2cc64f11
http://id.nii.ac.jp/1696/00037762/

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Unsteady Wing- Pylon- Nacelle Interference in Transonic Flow

Autor: Dietz, Guido, Mai, Holger, Schröder, Andreas, Klein, Christian, Moreaux, N., Leconte, P.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::dd52b0a1d7b94639975b87df5c4dfb9a
https://elib.dlr.de/54304/

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Numerical Simulation of Steady and Unsteady Aerodynamics of the WIONA (Wing with Oscillating Nacelle) Configuration

Autor: R. Voss, T. Tefy, A. Soda

Publikováno v: New Results in Numerical and Experimental Fluid Mechanics V ISBN: 9783540332862

This paper prresents an overview of numerical simulations on unsteady wing nacelle interference for the generic WIONA configuration. The geometry of the model exhibits typical aeordynamic interference effects, including the appearence of a shock in t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1ec5e2f03cd0a305577698b611729119
https://doi.org/10.1007/978-3-540-33287-9_41

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Dissertation/ Thesis

Análise experimental e teórica do efeito de uma Nacele \'Pusher\' nas características aerodinâmicas de um avião bimotor

Autor: Paulo Henrique Palota

Publikováno v: Biblioteca Digital de Teses e Dissertações da USPUniversidade de São PauloUSP.

Externí odkaz: http://www.teses.usp.br/teses/disponiveis/18/18135/tde-17022016-123236/

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Numerical Investigation of Wing-Nacelle Interference Effects at Transonic Flow Conditions for a Generic Transport Aircraft Configuration

Autor: Ante Soda, Tiana Tefy

Publikováno v: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783642535468

A detailed numerical and experimental investigation of the steady/unsteady wingpylon-nacelle interference effects on flutter characteristics has been initiated between DLR and ONERA. This paper presents preliminary numerical simulation results of ste

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f039a175a516a569b423847445121d32
https://doi.org/10.1007/978-3-540-39604-8_11

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An application of numerical optimization to a wing twist of SST wing-nacelle configuration

Autor: Yamazaki, Tetsuo, Saito, Mitsuru

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop). :325-326

航空宇宙技術研究所 17-19 Jan. 2000 東京日本
National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan
航空機の設計では、風洞試験やCFD(計算流体力学)法および他の評価法により、様々な機体形�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::16d4abfa69bb096307af3d36bffc4a10
http://id.nii.ac.jp/1696/00005762/

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