Accession Number:

AD0092459

Title:

FLIGHT TEST RESULTS ON THE USE OF HIGH LIFT BOUNDARY LAYER CONTROL APPLIED TO A MODIFIED LIAISON AIRPLANE

Descriptive Note:

Final summary rept.

Corporate Author:

CESSNA AIRCRAFT CO WICHITA KS

Report Date:

1956-03-31

Pagination or Media Count:

87.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE