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| /*===================================================================*/
/* NRDF D0043 Data No.60 */
/*===================================================================*/
/* Bibliography */
/*===================================================================*/
\\BIB,60;
D#=D43;
TITLE=/ALPHA-TRANSFOR REACTIONS BETWEEN 1P OR 2S-1D SHELL NUCLEI/;
PURPOSE=/TO STUDY THE MECHANISM OF THE ALPHA-TRANSFER REACTION/;
ATH=(T.MOTOBAYASHI'1');
INST-ATH=(2JPNIPC'1');
REF=IPC;
VLP=53(1977)81;
RCTS=(16O(14N,14N)16O, 16O(16O,16O)16O, 16O(10B,10B)16O,
16O(12C,12C)16O, 20NE(16O,16O)20NE,20NE(12C,12C)20NE,
20NE(10B,10B)20NE,10B(14N,14N)10B, 20NE(16O,15N)21NA,
16O(12C,11B)17F, 16O(16O,15N)17F, 16O(14N,13C)17F,
16O(14N,15O)15N, 10B(14N,13C)11C, 10B(14N,12C)12C,
16O(14N,12C)18F, 16O(14N,16O)14N, 10B(14N,11B)13N,
20NE(16O,20NE)16O,16O(16O,12C)20NE, 16O(12C,16O)12C,
16O(14N,10B)20NE, 12C(14N,10B)16O, 10B(14N,10B)14N,
16O(14N,9BE)21NA, 16O(14N,6LI)24MG, 12C(14N,9BE)17F,
12C(14C,7BE)19F, 10B(14N,9BE)15O, 10B(14N,7BE)17O);
/*===================================================================*/
/* Experimental Conditions */
/*===================================================================*/
\\EXP,60;
ENR=NAT;
CHM=GAS;
THK-TGT=40TORR;
BAC=SELF;
POL-TGT=NO;
ALGN-TGT=NO;
ACC=(CYC);
INST-ACC=2JPNIPC;
INC-ENGY-RANGE=(76.2MEV);
DELTA-INC-ENGY=300KEV;
ERS-PRJ=400KEV;
BEAM-INTNSTY=0.1UA;
POL-PRJ=NO;
DET-PARTCL=((16O,15O,14N,13C,12C,10B,9BE,6LI));
DET-SYS=(SI,CNTR-TLSCP);
SOLID-ANGL=0.2MSR;
ERS-DET=500KEV;
ANL=(OPT-MODEL,DWBA,STATIST-MODEL);
PHQ=(XSECTN,ANGL-DSTRN,OPT-POTL-PARA,SPEC-FCTR,J-CRITICAL);
/*CRITICAL ANGULAR MOMENTUM*/
RCT=16O(14N,14N)16O;
/*===================================================================*/
/* Descriptive Parameters */
/*===================================================================*/
\\DATA,60;
PRJ=14N;
TGT=16O;
INC-ENGY=76.2MEV;
POTL-FORM=/
-V*F(XR)-I*WV*F(XIV)+UC(R)
: F(XI)=1/(1+EXP(-XI))
: XI=(R-RI*(AT**(1/3)+AP**(1/3)))/AI
: UNIFORM CHARGE OF RADIUS RC*(AT**(1/3)+AP**(1/3)):/;
/*AT...MASS NUMBER OF TARGET ; AP...MASS NUMBER OF PROJECTILE*/
/*===================================================================*/
/* Data Table */
/*===================================================================*/
\DATA;
INC-ENGY V RR AR WV RIV AIV RC
(MEV) (MEV) (FM) (FM) (MEV) (FM) (FM) (FM)
76.2 134 0.92 0.77 40 1.29 0.328 1.3
\END;
/*===================================================================*/
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