1968
DOI: 10.1017/s0001924000084037
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Subsonic Aircraft Drag: An Appreciation of Present Standards

Abstract: Summary The drag at cruise CL of a number of recent aircraft—mostly large subsonic transports—has been analysed in terms of figures-of-merit derived from Melvill Jones’ original concept of a streamline aeroplane. The values have been compared with those for some representative aircraft from the 1930-1940 period. The paper then proceeds to highlight some of the main sources of excess drag; for the recent aircraft, these are grouped under broad headings such as “excrescences”, “Mach-number effects” a… Show more

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Cited by 8 publications
(5 citation statements)
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References 5 publications
(8 reference statements)
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“…9. The subsonic data do not appear to lend themselves to analysis in the form of equation (1). As can be seen in Figs.…”
Section: Stub Wingsmentioning
confidence: 88%
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“…9. The subsonic data do not appear to lend themselves to analysis in the form of equation (1). As can be seen in Figs.…”
Section: Stub Wingsmentioning
confidence: 88%
“…For cylinders which extend further into the boundary layer though still within a region characterised by the wall variables, hid becomes an important parameter because of the formation of horse-shoe vortices. For such cases a wallvariable relationship may be more appropriate than the form given by equation (1). Results in this form are given in Fig.…”
Section: Circular Cylindersmentioning
confidence: 99%
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“…Haines* 13 ' gave an account of subsonic aircraft drag, comparing post war progress with pre-war technology levels. He reviewed the drag of a number of transport aircraft.…”
Section: Background 21 Excrescence Dragmentioning
confidence: 99%
“…A. B. Haines (12) initiated a much needed revival of interest in subsonic drag in 1968 when much of the country's effort and attention was focused on supersonic and hypersonic flight. With limited resources such choices, although difficult, must sometimes be faced.…”
Section: Zone S-future Historicmentioning
confidence: 99%