Accession Number:

AD0676576

Title:

CALIBRATION MODELS FOR DYNAMIC STABILITY TESTS,

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1968-01-01

Pagination or Media Count:

8.0

Abstract:

This report describes three calibration models in the AGARD series. Model G A slender wing. Suitable for tests over a wide speed range. Fitted with a fin and a sting fairing. Model H A thin tapered wing suitable for high speed tests. Model J A 10 degree semi-angle cone, suitable for high supersonic speed testing. Author

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE