Microstructural refinement of W-Ni-Fe heavy alloys by alloying additions
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C o r r e c t i o n to Metall. Trans. A, 1988, vol. 19A, pp. 915-23
Orientation Dependence of t91 ~ 19~ Stress-induced Martensitic Tran,~formation in a Cu-AI-Ni Alloy by H. t i o r i k a w a , S. Ichinose, K. Morii, S. M i y a z a k i , and K. Otsuka
Page 918: The correct form o f Table IV is: Table IV.
The Values of Wj Calculated for 12 Correspondence Variants ( x l 0 -2)
Sp. No. Variant
3
4
5
9
10
12
13
15
1 1' 2 2' 3 3' 4 4' 5 5' 6 6'
4.234 4.234 1.259 1.259 -0.343 -0.343 i .034 1.034 -4.010 -4.010 -2.633 -2.633
5.111 5.111 1.506 1.506 -1.347 - 1.347 -0.588 -0.588 -2.507 -2.507 -1.748 - 1.748
5.462 5.462 2.542 2.542 0.303 0.303 0.988 0.988 -4.020 -4.020 -3.335 --3.335
5.864 5.864 4.596 4.596 3.727 3.727 4.127 4.127 -6.787 -6.787 -6.386 -6.386
4.342 4.342 1.448 1.448 -0.121 -0.121 1.208 1.208 - 4 . 178 -4.178 -2.849 -2.849
3.095 3.095 1.043 1.043 1.016 1.016 3.042 3.042 -5.752 -5.752 -3.727 -3.727
5.422 5.422 2.872 2.872 1.058 1.058 1.797 1.797 -4.764 -4.764 -4.024 -4.024
4.565 4.565 3.292 3.292 3.199 3.199 4.379 4.379 -6.933 -6.993 -5.812 -5.812
Sp. No. Variant
16
17
18
19
20
21
22
23
24
! 1' 2 2' 3 3' 4 4' 5 5' 6 6'
4.150 4.150 1.041 ! .041 -0.669 -0.669 0.734 0.734 -3.722 -3.722 -2.319 -2.319
1.854 1.854 -0.909 -0.909 - 1.092 - 1.092 1.488 1.488 -4.206 -4.206 - 1.626 - 1.626
1.744 1.744 - 1.134 - 1.134 - 1.397 - 1.397 1.219 1.219 -3.940 -3.940 - 1.325 - 1.325
4.147 4.147 1.044 1.044 -0.657 -0.657 0.749 0.749 -3.736 -3.736 -2.330 -2.330
5.238 5.238 2.589 2.589 0.779 0.779 1.621 1.621 -4.599 -4.599 -3.756 -3.756
6.507 6.507 3.794 3.794 1.171 1.171 1.123 1.123 -4.142 -4.142 -4.190 -4.190
5.968 5.968 5.758 5.758 5.643 5.643 5.739 5.739 -8.035 -8.035 -7.939 -7.939
3.314 3.314 1.384 1.384 1.366 1.366 3.278 3.278 -5.979 -5.979 -4.068 -4.068
4.511 4.511 3.288 3.288 3.269 3.269 4.474 4.474 -7.070 -7.070 -5.865 -5.865
Page 917: Line (or Eq.)
Original
Corrected
Eq. 121
W I -- 0-tT/t + 0"27/2 -t- 0"37/3
W l = o-t~ ~ + 0-2E~_ + 0-3E3
Line 16
for the d e f o r m a t i o n B~.
and e, = r h - l ( i
Line 11 (from the bottom)
(Table IV). W e see that . . . plane variant.
W e see that the variants are the largest for variants 1 and 1' in all s p e c i m e n s (Table IV). On the other hand, the o b s e r v e d variant is always 1'. This means that an applied stress interacts with thc shape strain rather than with B~ in the selection o f a habit plane variant.
METAI,I.URGICALTRANSACTIONSA
= 1 ~ 3).
VOLUME 20A, APRIL 1989--779
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