Heat reduction using conterflowing jet for a nose cone with aerodisk in hypersonic flow
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference34 articles.
1. Final report: on the structure of jets from highly underexpanded nozzles in to still air;Adamson,1958
2. Drag reduction using aerodisks for hypersonic hemispherical bodies;Ahmed;J. Spacecr. Rockets,2010
3. Metamodels for aerothermodynamic design optimization of hypersonic spiked blunt bodies;Ahmed;Aerosp. Sci. Technol.,2010
4. Unsteady separated supersonic flow over pointed and spiked bodies;Antonov;Fluid Dyn.,1974
5. Experimental investigation of the characteristics of unsteady-state breakaway zones arising in a supersonic flow at a needle with a screen;Antonov;Fluid Dyn.,1977
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