Free-flight model dynamic stability measurements on a 'not-so-slender' wing/fin combination at zero and small lift, M = 0.8 to 2.0.
Greenwood, G. H.,author.
Edwards, Geraldine F.,author.
Great Britain.Ministry of Defence,issuing body.
Great Britain.Her Majesty's Stationery Office.
Aeronautical Research Council (Great Britain)
"April 1974."