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DOE-STD-3014-96
APPENDIX B
WS/2
L
R
W
WS/2
H cot φ
WS
S
DIRECTION OF
CRASH
FIGURE B-3. Rectangular facility effective target area elements
Aeff
Af
As
(B-3)
where:
2 L W WS
Af
(WS R) H cot
LW
(B-4)
R
and
AS
(WS R) S
(B-5)
where:
Af
=
effective fly-in area;
As
=
effective skid area;
WS
=
aircraft wingspan, provided in Table B-16;
length of the diagonal of the facility, = (L2 + W2)0.5
R
=
B-27


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