Accession Number : AD0037709


Title :   THE EFFECT OF AN AXIALLY SYMMETRIC FUSELAGE ON THE NONSTATIONARY SUPERSONIC AIRLOADS ACTING ON A WING WITH SUPERSONIC EDGES


Descriptive Note : Technical rept.


Corporate Author : AERONAUTICAL SYSTEMS DIV WRIGHT-PATTERSON AFB OH FLIGHT CONTROL LAB


Personal Author(s) : EPSTEIN, MELVIN


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/037709.pdf


Report Date : May 1954


Pagination or Media Count : 45


Descriptors :   *SUPERSONIC CHARACTERISTICS , *WINGS , *FLUTTER , FUSELAGES , LOAD DISTRIBUTION , SUPERSONIC FLOW


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE