Advanced method for computing the flow around wings with rear separation and ground effect
By: Klaus Jacob.
Contributors: Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt.
Publisher: DFVLR Institut fur Theoretische Stromungsmechanik
Published: 1986
Place of publication: Gottingen
Number of pages: 62
Subjects: Ground effect (Aerodynamics); Separated flow; Subsonic flow; Wings
Notes: Bibliographical references: p.39-41.