Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
By: Krishnaswami Yegna Narayan and Klaus Hartmann.
Contributors: Hartmann, Klaus.; Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt.
Publisher: DFVLR
Published: 1988
Place of publication: Koln
Number of pages: 64
Subjects: Delta wings; Leading edges
Notes: Bibliographical references: p.25-27.