Accession Number:

AD0607552

Title:

GENERALIZED MISSILE DYNAMICS ANALYSIS. III. AERODYNAMICS,

Descriptive Note:

Corporate Author:

TRW SPACE TECHNOLOGY LABS LOS ANGELES CALIF

Personal Author(s):

• MILES,J. W.
• Young,Dana

Report Date:

1958-04-07

Pagination or Media Count:

18.0

Abstract:

The aerodynamic forces acting on a missile in consequence of small perturbations from a prescribed trajectory are calculated on the basis of slender body theory and piston theory is applied, in some detail, to the specific example of Generalized Missile Dynamics Analysis, II Equations of Motion.

Descriptors:

• AERODYNAMIC CHARACTERISTICS
• GUIDED MISSILES
• TRAJECTORIES
• MATHEMATICAL ANALYSIS
• EQUATIONS
• SLENDER BODIES
• PERTURBATION THEORY

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE