An Analytic Investigation of Accuracy Requirements for Onboard Instrumentation and Film Data for Dynamically Scaled Wind Tunnel Drop Models

Abstract

An analytic study was conducted to evaluate anticipated ranges and required accuracies for onboard linear acceleration and angular rate (or acceleration) measurement equipment to be mounted within dynamically scaled wind tunnel drop models. Generic simulations of the separation motion of a tumbling fuel tank both at full scale and at 1/15th wind tunnel model scale were generated using an analytic trajectory simulation program coupled with a prescribed aerodynamic database. The simulations provide a basis for sizing the required instrumentation for proof of concept demonstrations of telemetry techniques in the wind tunnel. The simulations were also used as test cases to demonstrate extraction of aerodynamic information from drop data positions and orientations as read from film records via an inverse solution of the store equations of motion. The studies also aid identification and evaluation of inaccuracies associated with the basic dynamic scaling laws and standard film based data reduction techniques.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1997
Accession Number
ADA322893

Entities

People

  • C. H. Morgret
  • K. S. Keen
  • R. L. Arterbury

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Angular Motion
  • Data Reduction
  • Digital Data
  • Equations
  • Equations Of Motion
  • Fuel Tanks
  • Instrumentation
  • Measurement
  • Orientation (Direction)
  • Physical Properties
  • Scaling Laws
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnel Models
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Dynamics.
  • Sensor Fusion and Tracking Systems.