gambit
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Try this source...Could you explain how that is applicable here (it is only true with jf-17 because it needs to redirect incoming air to the jet engine but not the other planes IMHO):
Infact the nose probably can never have the same surface area as the anywhere else along the fuselage. What you are saying is basically a cylinder, if you add a cone on top for piercing thru air, then you have something like a marker shaped Agni 3. The idea in a missile must be to create minimum turbulence while it is flying in the atmosphere and has very little need for maneuvering. Not sure how the same principle applies to a/c, if what you say was true there would be no canards esp. and other control surfaces to steer the plane.
Aerospaceweb.org | Ask Us - Area Rule and Transonic Flight
The 'nose' section of any aircraft include the cockpit area and for some even the canards, if so equipped. That mean it is not possible to change radome shape and dimension without a redesign of the 'nose' section and STILL maintain the original flight characteristics.What Whitcomb discovered was that the addition of wings to the basic cylinder produced twice as much drag as the cylinder alone. He also found that drag rose by the same amount if a simple bulge were added to the cylinder, the bulge being of equivalent volume as the wings. However, if he reduced the cross-sectional area of the fuselage over the region were the wings were attached, shown as body "D," the total drag was about the same as that of the cylinder alone.
The conclusion of this research was that shaping the vehicle to create a smooth cross-sectional area distribution from the nose to the tail could drastically reduce the drag on an aircraft. The area rule tells us that the volume of the body should be reduced in the presence of a wing, tail surface, or other projection so that there are no discontinuities in the cross-sectional area distribution of the vehicle shape.