WIND TUNNEL TEST REPORT CONVENTIONAL MODEL. VOLUME 2. LOW SPEED PRESSURE AND HINGE MOMENTS
GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT
Pagination or Media Count:
The report presents the results from wind tunnel tests of a one- eighth scale conventional model of the U. S. Army XV-5A Lift Fan Flight Research Aircraft. Volume II presents hinge moment coefficients and pressure data in plotted and tabular form with pertinent detail explanatory information. Pressure and hinge moment data were not recorded during the second phase of the low speed testing.
- Research and Experimental Aircraft