국내 최대 기계 및 로봇 연구정보

공학설계D/B

공학설계D/B 게시판 내용
Volume Title	Aerodynamics
Volume No	BODIES - Drag
DATA Title	Profile drag of axisymmetric bodies at zero incidence for subcritical Mach numbers.
DATA Item	78019
KEYWORD	afterbody, axisymmetric, body, cylinder, drag, forebody, geometry, profile, transition
ISBN	0 85679 221 7
ABSTRACT	ESDU 78019 gives a correlation of computed results using a method that allows iteratively for the displacement effects of the boundary layer and wake. It is found that by plotting the profile drag of the body as a fraction (the form factor) of the skin friction on a flat plate with the same transition position at the same Reynolds and Mach numbers, the data can be correlated and shown graphically simply as a function of body geometry parameters for a datum condition of transition at the nose, zero Mach number and fixed Reynolds number. Correction factors, also given graphically, correct the data for different transition positions and Mach numbers from datum. To assist in obtaining the value of profile drag, additional graphs give the flat plate mean skin friction for an appropriate range of transition positions, Reynolds numbers and Mach numbers. The method of correlating the data has been found to be accurate within 1 per cent for a range of body geometry and flow conditions. The computational method itself was found to agree within 5 per cent with a limited number of reliable experimental data available in the literature. A worked example illustrates the use of the data. ESDU 77028 gives, for a range of forebody and afterbody shapes, the geometry parameters required for the use of the correlation. Although the method is relatively simple to apply, it is fairly time consuming to evaluate by hand due to the need to determine some second-order effects of body geometry. Analytic equations were therefore developed using the original database. They are easily programmed and give a correlation only marginally worse than the graphical method and, moreover, they extend the method to cover a greater range of transition positions. It is tentatively suggested the method may be applied to bodies of smooth non-circular cross section.