Accession Number : AD0600502

Title :   A CRUCIFORM WING OF FINITE SPAN IN A COMPRESSIBLE FLOW.

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Fridlender,B. I.

Report Date : 13 APR 1964

Pagination or Media Count : 9

Abstract : The aerodynamic characteristics of a thin, cruciform wing consisting of four consoles of arbitrary geometric form are mathematical analyzed.

Descriptors :   (*CRUCIFORM WINGS, COMPRESSIBLE FLOW), (*COMPRESSIBLE FLOW, CRUCIFORM WINGS), SUPERSONIC FLOW, AERODYNAMIC CHARACTERISTICS, EQUATIONS, MATHEMATICAL ANALYSIS, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE