Accession Number:

AD0093275

Title:

FLIGHT INVESTIGATION OF THE EFFECT OF A PROPULSIVE JET POSITIONED ACCORDING TO THE TRANSONIC AREA RULE ON THE DRAG COEFFICIENTS OF A SINGLE-ENGINE DELTA-WING CONFIGURATION AT MACH NUMBERS FROM 0.83 TO 1.36

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1956-04-13

Pagination or Media Count:

45.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE