Accession Number:

ADA011288

Title:

Aeroloading and Dynamics of a Conical Vehicle During Pentration of a Blast Wave.

Descriptive Note:

Final rept. 1 Jan-31 Mar 74,

Corporate Author:

AUBURN UNIV ALA THERMOSCIENCE GROUP

Personal Author(s):

Report Date:

1974-04-01

Pagination or Media Count:

26.0

Abstract:

The report deals with the procedure for predicting transient loads on a conical vehicle during the oblique penetration of a blast induced shock wave. The importance of this analysis is in the application of the predicted aerodynamic loads to estimate the dynamic response of the missile during the blast penetration transient.

Subject Categories:

  • Aerodynamics
  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Explosions
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE