Accession Number:

AD0305630

Title:

INVESTIGATION OF THE INTEGRATED WING-DIFFUSER PRINCIPLE AT MISSILE DESIGN MACH NUMBERS OF 2.7 AND 3.5

Descriptive Note:

Corporate Author:

JOHNS HOPKINS UNIV LAUREL MD APPLIED PHYSICS LAB

Personal Author(s):

• BRUMBAUGH, V.W.
• PHELPS, C.M.

Report Date:

1958-04-01

Pagination or Media Count:

45.0

Abstract:

Descriptors:

• *GUIDED MISSILES
• *JET PROPULSION
• *SUPERSONIC DIFFUSERS
• DOWNWASH
• RAMJET INLETS
• SUPERSONIC FLOW

Subject Categories:

• Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE