Experimental Characterization of the Base Flow of a Slender Cone at Supersonic Speeds
Author:
Affiliation:
1. Florida State University
2. Florida State University Florida Center for Advanced Aero Propulsion
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1191
Reference14 articles.
1. Stivers, L. S. "Calculated Pressure Distributions and Components of Total-Drag Coefficients for 18 Constant-Volume, Slender Bodies of Revolution at Zero Incidence for Mach Numbers From 2.0 to 12.0, With Experimental Aerodynamic Characteristics for Three of the Bodies," , 1971.
2. Effects of Boattailing on the Turbulence Structure of a Compressible Base Flow
3. Visualization of a central bleed jet in an axisymmetric, compressible base flow
4. A review and development of correlations for base pressure and base heating in supersonic flow
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1. Base Flow Measurements of a Slender Cone at Mach 6;AIAA SCITECH 2024 Forum;2024-01-04
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