Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume II.
CALSPAN CORP BUFFALO N Y
Pagination or Media Count:
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.
- Guided Missile Dynamics, Configurations and Control Surfaces
- Guided Missiles