ADMITTANCE TECHNIQUES IN HIGH SPEED FLUTTER MODEL TESTING. PART 2. CORRELATION OF EXPERIMENT AND THEORY

Abstract

A comparison of experimental and theoretical flutter results for a wing-body configuration in the supersonic speed regime is presented. The experimental flutter results were obtained by application of admittance techniques and are free flight data. Piston theory and Mach box calculations at a Mach number of 1.5 agree quite well with the experimental results. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1961
Accession Number
AD0325438

Entities

People

  • Gifford W. Asher

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Flight
  • Fluid Dynamics
  • Free Flight
  • Mach Number
  • Wing Body Configurations

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow