what would be the most appropriate choice for the bulk material used for a turbine blade in a jet engine?
what would be the most appropriate choice for the bulk material used for a turbine blade in a jet engine?
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Question

Transcribed Image Text:Using the Ashby chart below (also
given in class),
Strength - Max service temp.
Carbon Cost Low aloy Ti aloys
Ses irore soels
Stainless
sloels
CFRP
Ni alóys
Walloys
Mg aloys
Al alloye
Cu ellays
SiNa
1000
Metals
Zinc aloys
Nyors
PET
PUMA
AIN
100
GFR
ea glase
PVC -
ANS
PEEK
Soda gloss
Borosilicate glas
Technical
ceramics
pp poces
Neoprone
Louhey
10
Brick
Lead alloys
EVA
PTFE
Stone
lonomers
Wood
Polymers and
elastomers
Scone
elastomers
Non-technical
ceramics
Rgd palymer
foams
Coscrete
Buta rubber
Cork
Foams
01
Fexble polymer
foams
MEA 4
0.01
10
100
Maximum service temperature, Tmax (°C)
30
300
1000
what would be the most appropriate
choice for the bulk material used for a
turbine blade in a jet engine?
O Al203
Nickel alloys
Carbon fibre composite
O Kevlar
Strength, of (MPa)
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