An Evaluation of Structural Damage (Window Breakage) Potential in Callente, NV Under Current Supersonic Flight Restrictions at Nellis AFB.

Abstract

During November 1996 a series of tests was performed in and around Caliente, NV. These tests, performed by the firms of Cambridge Acoustical Associates, Inc., and Wyle Laboratories, Inc., are part of a Small Business Innovative Research (SBIR) project, being sponsored by the Armstrong Laboratory of the United States Air Force. The project objective is to perfect measurement techniques that simulate structural response to sonic booms, and in turn allow one to assess potential damage, especially to unconventional structures. The goals of the Caliente tests were twofold. The first was to provide additional data for the validation of the techniques. The second was to demonstrate the process by which such measurements may be used to perform an environmental (structural) damage assessment. This report focuses on the latter. To limit the overall environmental impact on Caliente, supersonic operations from Nellis AFB have recently been prohibited within five miles of the town. To evaluate the adequacy of this restriction with respect to avoiding structural damage, window damage to be exact, a part of our test plan was devoted to a measurement survey of various windows throughout the town. From these data we have simulated their peak response (stress) to the sonic boom environment evaluated under the above mentioned flight restriction. Twenty windows were tested, including those of a number of commercial buildings, the library, train station, and one of the auxiliary hospital buildings. (Window installations with a noticeable rattle are not readily simulated and were excluded from the ensemble.) Based on our simulations (Table 3), the least susceptible to damage is a window of the Bureau of Land Management (BLM) Building and a train station window is the most vulnerable. For all windows, no additional breakage is anticipated under current flight restrictions.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1997
Accession Number
ADA329470

Entities

People

  • J. M. Downing
  • Joel Garrelick
  • Kyle Martini
  • Ron Brown

Tags

Communities of Interest

  • Biomedical
  • Sensors

DTIC Thesaurus Topics

  • Air Force
  • Damage Assessment
  • Databases
  • Environment
  • Environmental Health
  • Flight
  • Frequency
  • Hospitals
  • Mach Number
  • Measurement
  • Noise
  • Simulations
  • Sonic Boom
  • Supersonic Flight
  • United States
  • Vibration
  • Waves

Readers

  • Aviation Science / Aeronautics.
  • Coastal and Marine Engineering/Sediment Transport/Hydraulic Engineering
  • Facility/Structural Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow