Force and Pressure Tests of a Six Caret-Wing-Body Model,
CORNELL AERONAUTICAL LAB INC BUFFALO N Y
Pagination or Media Count:
Tests to determine six-component force and pressure distribution data on a six caret-wing-body model were performaned in a hypersonic shock tunnel. The report presents the details of the test program, a description of the model and equipment used, and a tabular and graphic presentation of obtained data.
- Fluid Mechanics