Accession Number:

AD0784259

Title:

A Study of the Damping Characteristics on Models of Supersonic Airlines at Supersonic Speeds,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-07-24

Pagination or Media Count:

11.0

Abstract:

The article presents the results of an experimental study of the damping moment coefficients of the configuration of supersonic airliner models with small wing aspect ratios in a supersonic wind tunnel. A comparison of experimental and calculated data is presented.

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE