The Stability of Motion of Parachute in the Steady-State Reduction Mode,

Abstract

The stability conditions of the plane oscillation of a parachute are examined under the conditions of the reduction made, taking into account the virtual inertia effect of air.

Document Details

Document Type
Technical Report
Publication Date
Jan 24, 1975
Accession Number
ADA007183

Entities

People

  • A. A. Shilov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boat And Ship Safety
  • Oscillation
  • Parachutes
  • Stability Conditions
  • Steady State

Readers

  • Aerial Delivery - Logistics and Supply Chain Management.
  • Structural Dynamics.