Accession Number : ADA195832

Title :   Kinetic Energy Finned Projectile Aerodynamic Heating Measurements.

Descriptive Note : Interim rept. no. 2,

Corporate Author : DEUTSCHE FORSCHUNGSANSTALT FUER LUFT- UND RAUMFAHRT E V BRUNSWICK (GERMANY F R) INST FUER FLUGMECHANIK

Personal Author(s) : Schoeler, H

PDF Url : ADA195832

Report Date : 14 Apr 1987

Pagination or Media Count : 3

Abstract : Designing of the models is finished. A sketch of the models is shown. Three forebodies can be screwed to the model or, for observation of the nose region, to a short sting mounted in the model support of the Ludwieg tube. The fins will be glued into slits in the main support sting. All parts except the two stings will be machined from Plexiglas. Keywords: Wind Tunnel; Models. (jhd)

Descriptors :   *WIND TUNNEL MODELS, BITES AND STINGS, FINS, MODELS, NOSES, REGIONS, WIND TUNNELS

Subject Categories : Test Facilities, Equipment and Methods
      Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE