Guided weapons aerodynamic study
Subtitle: preliminary analysis of the characteristics of wing tip, trailing edge and aft-mounted control surfaces on a monoplane delta wing-body combination of aspect ratio 0.83 at Mach numbers from 0.6 to 2.8.
Contributors: Royal Aircraft Establishment (Great Britain)
Series: Tech. memo. Aero -- 962; Technical memorandum (Royal Aircraft Establishment (Great Britain)) -- P 962.
Publisher: Royal Aircraft Establishment
Published: 1966
Place of publication: (Farnborough)
Language: eng
Number of pages: 29