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- W163934359 abstract "Wind tunnel force and moment measurements are presented for a body at Mach numbers between 0·6 and 2·8 and for three body-wing configurations, which have the same span but different wing-root chord lengths, at Mach numbers between 1.3 and 2·8 for a Reynolds number of 2 million per foot. The body, of overall fineness ratio 13 and nose fineness ratio 3, is common to all configurations.Tbe body alone results show that the longi tudinal forces and moments have large non-linear components. A comparison of experimental and estimated results shows rather better agreement at the higher than at the lower Mach numbers. The results for the body-wings show toot for the normal force variation with incidence, the degree of non-linearity decreases as Mach number increases. The centre of pressure moves significantly as Mach number, incidence and the nose length ahead of the wing-root leading-edge vary.Estimates of normal force and centre of pressure show good agreement with experimental results at all Mach numbers." @default.
- W163934359 created "2016-06-24" @default.
- W163934359 creator A5058583696 @default.
- W163934359 date "1965-06-30" @default.
- W163934359 modified "2023-09-26" @default.
- W163934359 title "Guided weapons aerodynamic study: a study on a body alone, and in combination with delta-wings of aspect ratios 0-83, 1-03 and 1-24 at mach numbers up to 2-8" @default.
- W163934359 hasPublicationYear "1965" @default.
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