Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing
By: by R. T. Griffiths.
Series: Aeronautical Research Council. Current papers,; no. 1059; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 1059.
Publisher: H.M. Stationery Off.
Published: 1969
Place of publication: London
Language: eng
Number of pages: 18
Subjects: Airplanes -- Nacelles.; Airplanes -- Wings.; Boundary layer.; Wind tunnels.
Notes: Includes bibliographical references.