Projectile with reduced base drag

• US 4,813,635 A
• Filed: 12/29/1986
• Issued: 03/21/1989
• Est. Priority Date: 12/29/1986
• Status: Expired due to Fees

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Werle, Michael J., Presz, Walter M. Jr., Paterson, Robert W.
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US06/947,163
• Time in Patent Office: 813 Days
• Field of Search: 244/130, 244/200, 244/199, 244/198, 244/3.1, 244/3.24, 244/3.23, 102/501, 102/385, 102/389, 416/236 A, 296/1 S
• US Class Current: 244/130
• CPC Class Codes: B62D 35/001 For commercial vehicles or tractor-trailer combinations, e.g. caravans
• CPC Class Codes: B62D 35/007 Rear spoilers B62D35/001 takes precedence
• CPC Class Codes: F42B 10/44 Boat-tails specially adapted for drag reduction
• CPC Class Codes: Y02T 10/82 Elements for improving aerodynamics

Abstract

A projectile having a downstream extending surface of revolution which terminates as a blunt base has a plurality of circumferentially spaced apart U-shaped, downstream extending troughs in its surface. Each trough is essentially aligned with the direction of the bulk fluid flow adjacent the surface in the vicinity of the trough, and intersects the blunt base to form a trough outlet therein. The troughs are appropriately spaced apart, sized and configured to flow full over their entire length and to cause fluid to flow into the space immediately behind the blunt base, thereby reducing base drag on the projectile.

Claims

1. A projectile adapted to travel through a fluid in an upstream direction, said projectile having an external surface which is substantially a surface of revolution about an axis extending in the upstream direction, said projectile having a blunt, downstream facing end surface, said surface of revolution terminating at said end surface, a plurality of circumferentially spaced apart downstream extending troughs formed in said surface of revolution, each trough being smoothly U-shaped in cross section along its length, having zero depth at its upstream end and blending smoothly at its upstream end with said external surface of revolution, and intersecting said end surface to form a smoothly U-shaped trough outlet, each of said troughs increasing in depth to a maximum depth at its outlet, wherein the contour and dimensions of said troughs are selected to ensure that each trough flows full throughout its length and generates a pair of large-scale, counterrotating vortices downstream of the trough outlet, the axes of the vortices extending in the downstream direction, whereby fluid is caused to flow into the space immediately downstream of said blunt end surface to reduce base drag.

2. The projectile according to claim 1, wherein the projectile is adapted to travel upstream and simultaneously rotate about its axis, wherein each of said troughs extends downstream substantially parallel to the direction of a vector which is the sum of a vector representing the axial velocity of the projectile and a vector representing the rotational velocity of said external surface at said trough outlet.

3. The projectile according to claim 1 wherein each of said troughs includes a pair of sidewall surfaces which face each other and which intersect said end surface to form side edges of said trough outlets, and the downstream projected area of the portion of the blunt end surface disposed circumferentially between said side edges of each pair of adjacent trough outlets is at least one quarter (1/2) of the downstream projected area of one of said adjacent trough outlets.

4. The projectile according to claim 3 wherein said plurality of troughs define a smoothly undulating surface which is wave-shaped in cross section perpendicular to the axial direction.

5. The projectile according to claim 4 wherein, in cross section perpendicular to the axial direction, lines tangent to each side wall of said pair of trough side walls at their steepest point at said trough outlet form an included angle of no more than 120°

.

6. The projectile according to claim 1 wherein each of said troughs includes a pair of sidewall surfaces which terminate as side edges at said trough outlet, said sidewall surfaces being substantially parallel to the direction of bulk fluid flow over the surface in which said trough is disposed over a substantially continuous portion of the length of said trough, including said trough outlet.

7. The projectile according to claim 4 wherein each of said troughs includes a pair of sidewall surfaces which terminate as side edges at said trough outlet, said sidewall surfaces being substantially parallel to each other at said trough outlet.

8. The projectile according to claim 7 wherein said sidewall surfaces are substantially parallel to the direction of bulk fluid flow over the surface in which said trough is disposed over a substantial continuous portion of the length of said trough, including said trough outlet.