Accession Number:

ADA160264

Title:

The Shock and Vibration Bulletin. Part 2. Dynamic Testing, Flight Vehicle Dynamics, Seismic Loads and Fluid-Structure Interaction

Descriptive Note:

Corporate Author:

NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER

Personal Author(s):

Report Date:

1985-06-01

Pagination or Media Count:

203.0

Abstract:

Symposium paper include Triaxial Vibration System Initial Design and Testing of a Unique High Frequency Fatigue Test System Investigation of Modes, Frequencies and Forced Response of a High Frequency Fatigue Test System Data Analysis Techniques to Support Structural Modeling Ultra-high Velocity Impacts Using Rocket Sled and an Explosively Accelerated Flyer Plate Water Impact Testing of a Filament Wound Case Airworthiness Flight Test Program of an Aircraft Equipment Fairing An Update of Spacecraft Dynamic Environments Induced by Ground Transportation Reliability of Structures Subjected to Multiple Blast Loads Shock Environment in a Civil Defense Blast Shelter Earthquake Induced Motion Environments in Framed Buildings Development of a 3KBAR Static Calibration Device DAlembert Unfolding of Hopkinson Bar Airblast Data Design and Field Experience with the WES 10KBAR Airblast and Soil Stress Gage Structural Response of Panels Subjected to Shock Loading Generalized Dynamic Analysis of Interactive Fluid-Structure Transient Response Field Experiences of UNDEX Testing for Stiffened Flat Plate Model and Analysis of Cavitation Caused by Shock Wave Interaction with a Restrained Mass.

Subject Categories:

  • Aircraft
  • Test Facilities, Equipment and Methods
  • Mechanics
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE