What is a Waverider?
When it comes
to generating Lift, the best supersonic aircraft shape is a simple wedge inclined at an angle
(known as the angle of attack) to the incoming air. The underside 'wedges'
into the air, compressing it to generate Lift. (The upper surface doesn't
do anything.) The wings and the fuselage are often blended together for
aircraft that travel at supersonic speeds, so the wedge is the whole
aircraft, not just the wings.
This diagram shows a
side view of the wedge, which is assumed to have infinite wingspan in the direction normal
to the page. This imaginary wedge, and the flow around it, are called ‘two
dimensional’, because there is no flow in the direction of the third
dimension, the direction normal to the page.
Just as
with real subsonic aircraft, the finite wingspan of a real supersonic aircraft causes
unwanted spanwise flow components (in the 3rd dimension) caused
by the wingtips.
These wing-spanwise
flows
degrade performance: some of the compressed underside air leaks out over
the wingtips and so some Lift is lost.
Waveriders
are any supersonic aircraft that have underside features designed to
minimise these spanwise flows and so retain as much of the underside Lift
as possible. They do this by having some underside concavity:
Concavity:
Imagine a typical
lifting-body toy model (e.g. a Space Shuttle) held upside-down and at an
angle under a running tap. The water will hit the underside and
spread out over the surface, but as well as running out over the back, the
water will also spill out over the edges because the underside is either
flat or convex: a spanwise flow is established:
This water flow
is more than just an analogy to supersonic airflow: the water reacts to
changes in height on the model undersides, exactly as airflow under the
real vehicle does. The Space Shuttle loses a 1/4 of its possible lift
due to underside air spilling sideways over the edges of its wings.
The
underside of a Waverider model is concave, therefore the water (airflow)
will tend to stay in the middle of the underside before running out over
the back, inhibiting spanwise flow and spillage.
The
two Waveriders shown opposite are deeply concave; the one on the right is
known as a 'Caret wing'
because when viewed
from the front it looks like your keyboard's caret symbol ^
Actually, only the underside areas near to the wing
leading edges need be concave to 'wall-in' the airflow; the underside of
the Caret wing for example can be filled-in to a large degree, which gives
more fuselage internal space, and a lower vehicle centre of gravity (CG)
to aid stability.

Some degree of concavity can be added to just about any
supersonic delta-winged aircraft; every little helps improve Lift. Both
the XB70 Valkerie supersonic bomber and the British TSR2 supersonic
aircraft had drooped wingtips to give a bit of underwing concavity:
Sharp edges:
The other feature that helps contain underside flow is a
sharp nose and leading edges. You'll have noticed that in contrast, the
Space Shuttle has very rounded nose and edges because of its thermal
protection ethos. This convexity at the edges just promotes spillage.
Waveriders typically employ sharp nose and wing leading
edges: shockwaves generated by a sharp edge appear to emanate directly
from the tip of the edge, and so a sharp-edged Waverider appears to ride
atop a shockwave attached to its edges: hence the name 'Waverider'.
For more information on Waveriders see our technical
papers page.
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