Accession Number:

AD0766661

Title:

Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume III.

Descriptive Note:

Technical rept.,

Corporate Author:

CALSPAN CORP BUFFALO N Y

Personal Author(s):

Report Date:

1973-07-01

Pagination or Media Count:

666.0

Abstract:

Volume 3 of a three volume report tabulates aerodynamic and thrust test data on a wind tunnel model of a guided missile with canard wings. Included are tail fin force and moment coefficients.

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE