Accession Number : AD0305630

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

Corporate Author : JOHNS HOPKINS UNIV LAUREL MD APPLIED PHYSICS LAB

Personal Author(s) : BRUMBAUGH, V.W. ; PHELPS, C.M.

Report Date : APR 1958

Pagination or Media Count : 45

Descriptors :   *GUIDED MISSILES, *JET PROPULSION, *SUPERSONIC DIFFUSERS, DOWNWASH, RAMJET INLETS, SUPERSONIC FLOW.

Subject Categories : Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE