About this document
Similarity Rules in Supersonic Flow by Arun Yoga is a document available to read on EtoBox.
Similarity rules allow aerodynamic characteristics like pressure coefficient (Cp) to be represented by a single curve across a range of Mach numbers and body shapes. Dimensional analysis identifies non-dimensional parameters, and similarity analysis groups these into similarity parameters to reduce the number of independent variables. For linearized supersonic flow over slender bodies, Cp remains invariant if thickness ratio (τ) is reduced as Mach number (M∞) increases to keep (1-M∞)2/2 constant. Göthet rul
- Author
- Arun Yoga
- Language
- EN