Fixed plane wave rider design method based on osculating cone theory
Patent Information
- Authority / Receiving Office
- CN Β· China
- Current Assignee / Owner
- CHINA ACAD OF AEROSPACE AERODYNAMICS
- Publication Date
- 2018-04-27
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Abstract
Description
technical field
[0001] The invention relates to the field of layout aerodynamic design of a hypersonic vehicle, especially the layout form of a waverider. Background technique
[0002] The high-lift supersonic / hypersonic shape has always been the relentless pursuit of human beings. According to the hyperbolic characteristics of hypersonic inviscid flow, the aerodynamic performance of the aircraft can be improved to a large extent, and the waverider is a typical shape that utilizes this characteristic. The waverider divides the high-pressure aerodynamics on the lower surface of the aircraft by attaching the shock wave to prevent flow leakage, effectively breaking through the lift-drag barrier of the hypersonic aircraft, and has a high lift-to-drag ratio. After decades of development, the waverider has gradually developed from a single configuration in the early stage to a complex configuration with different characteristics, especially the proposal of the close cone method, ...