NASA NTRS · 19700001663
An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack
Abstract
Incompressible approximation solution of additive drag coefficient and mass flow ratio for inlets with right circular cones
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Mascitti, V. R.. 1969-11-01. An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack. https://ntrs.nasa.gov/citations/19700001663
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