ASD Technical Report, Numéro 61,Partie 684Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962 |
Table des matières
INTRODUCTION | 1 |
Electrode Preparation | 7 |
EXTRUSION STUDIES | 19 |
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1V ALLOY 4200-cycle induction 50 per cent Alginate alloy compositions alloy shows annealed 1 hr Annealing Temperature argon as-extruded Battelle Battelle Memorial Institute bend and tensile BILLET ACCESSORIES BILLET Composition Billet Final Material Billet Precoat Material BILLET TRANSFER sec Bottom chamfer cold rolling contamination crucible diam diameter double-melted ingots ductility Elastic Modulus electrodes Elongation Extruded 4:1 EXTRUDED BAR EXTRUSION DATA SHEET extrusion ratio finish rolling grain Graphite hafnium HARVEY SERIAL HIGH-PRESSURE ADMISSION hour inch incl Ingot 1AB Ingot 1CD Ingot 1EF laminations Maximum ips Minimum ips Nose Block nose configuration Number radius RAM SPEED remelt rolled at 800 room temperature samples second phase SHEET BEND shown in Figure Side ips Side rolled single-melt ingots Straight rolled structure surface Ta-10Hf-5 W alloy Ta-10Hf-5W ALLOY INGOT Table Tantalum alloys TANTALUM-BASE ALLOYS Temperature 800 tensile properties tests transverse tungsten Type 90 Vacuum annealed Valve Setting turns vanadium welded Yield Strength ZrO2