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- W836766612 abstract "SUMMARY A parametric study was conducted to determine the theoretical aerodynamic characteristics of right circular cones modified to produce Lift at zero angle of attack. In the modification, portions of the cone lying above and behind an inclined plane surface were removed. Newtonian impact theory was used to express force and moment coefficients as functions of the manner in which the cone is terminated by this cutting plane at the base. In addition, relationships were formed that allow limits of acceptable design and performance characteristics to be imposed, such as lower limits of useful volume and lift-drag ratios, assurance of maintaining supersonic flow over the trailing edges, and the permissible range of center-of-gravity locations to assure trim at zero angle of incidence. The configurations studied sug gest that it is practical to trim cones at a useful level of lift-drag ratio without inclining the axis of the basic cone relative to the airstream. INTRODUCTION Vehicles returning to earth from space flights to nearby planets will enter the atmosphere at speeds considerably greater than returning lunar vehicles (up to twice" @default.
- W836766612 created "2016-06-24" @default.
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- W836766612 date "1969-05-01" @default.
- W836766612 modified "2023-09-27" @default.
- W836766612 title "Newtonian aerodynamics for circular cones modified to produce lift at zero angle of attack" @default.
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- W836766612 hasPublicationYear "1969" @default.
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