Accession Number:

AD0766660

Title:

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

Descriptive Note:

Technical rept.,

Corporate Author:

CALSPAN CORP BUFFALO N Y

Personal Author(s):

Report Date:

1973-07-01

Pagination or Media Count:

674.0

Abstract:

The report is Volume 2 of a three volume series. Tables of aerodynamic test data are given, including balance cavity and base pressure coefficients, axial force for aerodynamic and thrust phases, canard position, and force and moment coefficients for a series of runs.

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE