Transonic and supersonic flow past a 65° delta wing with rounded leading edges : analysis of experimental data; 1 table / Krishnaswami Yegna Narayan and Klaus Hartmann
Contributor(s): Resource type: Ressourcentyp: BuchBookLanguage: English Series: Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt. Forschungsbericht ; 1988,44Publisher: Köln : Wiss. Berichtswesen d. DFVLR, 1988Description: 64 SReport number: DFVLR-FB 88-44; DFVLR FB 88 44Genre/Form: Action note:- 3
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