Accession Number:

AD0404922

Title:

AERODYNAMIC COEFFICIENTS FROM SHOCK EXPANSION THEORY: ANALYTICAL DEVELOPMENT FOR PLANAR SURFACES

Descriptive Note:

Corporate Author:

AEROSPACE CORP EL SEGUNDO CA

Personal Author(s):

Report Date:

1963-04-29

Pagination or Media Count:

42.0

Abstract:

A simplified version of the shock expansion theory is employed to estimate the unsteady aerodynamic loading on a planar surface. Expressions for oscillatory aerodynamic coef ficients are developed for the case of a three degrees-of-freedom airfoil section.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE