A COMPARISON OF EXPERIMENTAL AND THEORETICALLY PREDICTED PRESSURE DISTRIBUTIONS AND FORCE AND STABILITY COEFFICIENTS FOR A SPHERICALLY BLUNTED CONE AT MACH APPROX. 18 AND ANGLES OF ATTACK
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
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Analysis of experimental pressure distributions and force and moment coefficients for a 9-deg half-angle spherically blunted cone is presented based on an ideal gas y 1.4 three-dimensional characteristics solution developed by General Applied Sciences Laboratory GASL. Comparisons are also made with predictions based on modified Newtonian theory.
- Military Aircraft Operations
- Fluid Mechanics