Accession Number:

AD0029316

Title:

ROCKET-MODEL INVESTIGATION OF THE LONGITUDINAL STABILITY, DRAG, AND DUCT PERFORMANCE OF A 60 DEGREE DELTA-WING CANARD AIRCRAFT WITH TWIN SIDE INLETS AT MACH NUMBERS FROM 0.80 TO 1.70

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1954-03-01

Pagination or Media Count:

55.0

Abstract:

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE