Catalogo Articoli (Spogli Riviste)

OPAC HELP

Titolo:
Inverse design of a thick supercritical airfoil
Autore:
Pambagjo, TE; Nakahashi, K; Obayashi, S;
Indirizzi:
Tohoku Univ, Dept Aeronaut & Space Engn, Sendai, Miyagi 980, Japan Tohoku Univ Sendai Miyagi Japan 980 Space Engn, Sendai, Miyagi 980, Japan
Titolo Testata:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
fascicolo: 140, volume: 43, anno: 2000,
pagine: 61 - 66
SICI:
0549-3811(200008)43:140<61:IDOATS>2.0.ZU;2-P
Fonte:
ISI
Lingua:
ENG
Keywords:
inverse design; supercritical airfoil;
Tipo documento:
Article
Natura:
Periodico
Settore Disciplinare:
Engineering, Computing & Technology
Citazioni:
8
Recensione:
Indirizzi per estratti:
Indirizzo: Pambagjo, TE Tohoku Univ, Dept Aeronaut & Space Engn, Sendai, Miyagi 980, Japan Tohoku Univ Sendai Miyagi Japan 980 endai, Miyagi 980, Japan
Citazione:
T.E. Pambagjo et al., "Inverse design of a thick supercritical airfoil", T JPN SOC A, 43(140), 2000, pp. 61-66

Abstract

In this paper, a study on designing a thick supercritical airfoil by utilizing Takanashi's inverse design method is discussed. One of the problems todesign a thick supercritical airfoil by Takanashi's method is that an oscillation of the geometry may occur during the iteration process. To reduce the oscillation, an airfoil parameterization method is utilized as the smoothing procedure. A guideline to determine the target pressure distribution to realize the thick airfoil is also discussed.

ASDD Area Sistemi Dipartimentali e Documentali, Università di Bologna, Catalogo delle riviste ed altri periodici
Documento generato il 07/07/20 alle ore 04:41:20