The impact of the length-to-depth ratio on aerodynamic surface quantities of a rarefied hypersonic cavity flow

Author:

Palharini Rodrigo C.ORCID,Santos Wilson F.N.ORCID

Funder

FAPESP

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference61 articles.

1. Drag Associated with Separated Flow Over Two-Dimensional V-Shaped Notches Under Transonic and Supersonic Conditions;Howell,1968

2. Drag of rectangular cavities in supersonic and transonic flow including the effects of cavity resonance;McGregor;AIAA J.,1970

3. Numerical simulation of flow over an airfoil with a cavity;Olsman;AIAA J.,2011

4. Effect of geometric parameters on the drag of the cavity flameholder based on the variance analysis method;Huang;Aerosp. Sci. Technol.,2012

5. Multi objective design optimization of the performance for the cavity flameholder in supersonic flows;Huang;Aerosp. Sci. Technol.,2013

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