这种格式如何转换成sql数据库格式

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我从一种数据库导出了一批数据格式如下：
Record 132828 in Database ENPS31199701
SEQNO : ZX1997027636
LAN : eng
TIT : Flap-Lag-Torsion Stability in Hover and Forward Flight with
Three-Dimensional Wake
PAGE : p.18-28
MTIT : AIAA Journal
MVOL : Vol.34, No.1 , 1996
CLASSNO : V; V2
AU1 : A. R. Manjunath, S. J. Chunduru, J. Nagabhushanam
LIBNO : CN111001
LIBCLASSNO: V1-25
LIBNUM : 4-1562
ZTNO : 877B0001
ISSN : 0001-1452
PYEAR : 1996
ID : 0001-1452(1996)l:1<18:FLTSIH>2.0.TX;2-J
MID : N200309508
RIDN : 132828
AB :
The contributions of full-wake dynamics in trim analysis are
demonstrated for finding the control inputs and periodic responses
simultaneously, as well as in Floquet eigenanalysis for finding the
damping levels. The equations of flap bending, lag bending, and
torsion are coupled with a three-dimensional, finite state wake, and
low-frequency (<l/rev) to high-frequency (>l/rev) multiblade modes
are considered. Full blade-wake dynamics is used in trim analysis and
Floquet eigenanalysis. A uniform cantilever blade in trimmed flight
is investigated over a range of thrust levels, advance ratios, number
of blades, and blade torsional frequencies.


Record 132829 in Database ENPS31199701
SEQNO : ZX1997027637
LAN : eng
TIT : Application of the Finite Element Method to Acoustic Scattering
Problems
PAGE : p.29-34
MTIT : AIAA Journal
MVOL : Vol.34, No.1 , 1996
CLASSNO : V; V2
AU1 : J. A. Eaton, B. A. Regan
LIBNO : CN111001
LIBCLASSNO: V1-25
LIBNUM : 4-1562
ZTNO : 877B0001
ISSN : 0001-1452
PYEAR : 1996
ID : 0001-1452(1996)l:1<29:AOTFEM>2.0.TX;2-2
MID : N200309508
RIDN : 132829
AB :
For aircraft, scattering of engine and rotor noise from the
fuselage and wings can considerably influence com- munity and
interior noise levels. Here the finite element method (FEM) is
considered as a modeling technique because of its ability to solve
for a broad range of governing equations and its potential efficiency
advantages over the more commonly used boundary element method. With
FEM, however, the data storage requirements become very demanding for
three-dimensional problems involving realistic geometries and
frequency ranges. To enable large FEM problems to be tackled using
relatively modest computing facilities, the computational cost is
addressed at several levels.


Record 132830 in Database ENPS31199701
SEQNO : ZX1997027638
LAN : eng
TIT : Matching Inviscid/Boundary-Layer Flowfields
PAGE : p.35-42
MTIT : AIAA Journal
MVOL : Vol.34, No.1 , 1996
CLASSNO : V; V2
AU1 : Fred R. DeJarnette, Robert A. Radcliffe
LIBNO : CN111001
LIBCLASSNO: V1-25
LIBNUM : 4-1562
ZTNO : 877B0001
ISSN : 0001-1452
PYEAR : 1996
ID : 0001-1452(1996)l:1<35:MIBLFM>2.0.TX;2-8
MID : N200309508
RIDN : 132830
AB :
New boundary-layer equations are developed and the solutions
match all of the boundary-layer properties, except for the normal
velocity, exactly with the corresponding inviscid properties. The
numerical procedure solves tridiagonal matrices at each marching
station. As part of the solution an inviscid transpiration velocity
at the surface is calculated from the boundary-layer solution. This
transpiration velocity could be used as a boundary condition to
calculate a new inviscid solution. If the inviscid/boundary-layer
solutions are interacted, then the normal velocity from the
boundary-layer solution will match the inviscid values exactly.
如何把这批利用sql的转换工具导入到sql的表里