Accession Number : AD0325438

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

Corporate Author : BOEING CO SEATTLE WA

Personal Author(s) : ASHER, GIFFORD W.

Report Date : JUL 1961

Pagination or Media Count : 1

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)

Descriptors :   *FLUTTER, *JET AIRCRAFT, *WING BODY CONFIGURATIONS, AERODYNAMIC CHARACTERISTICS, MATHEMATICAL ANALYSIS, SUPERSONIC FLOW.

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE