umwelt-online: VBUF - Vorläufige Berechnungsmethode für den Umgebungslärm an Flugplätzen - VBUF-AzB

Flugzeugklasse S 2 - Ab

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	95,5	1,2
2	102,0	1,2
3	102,0	1,2
4	100,0	1,2
5	97,0	1,1
6	93,0	1,0
7	89,0	1,0
8	73,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	40	0
1.300	0	80	0
3.600	0	80	-
4.100	-	80	460
4.600	- 3	80	-
7.800	- 3	80	920
18.800	- 3	135	1.283
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 18.800	0	0	0,033

Flugzeugklasse S 2 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	81,0	1,2
2	83,5	1,2
3	85,0	1,2
4	83,0	1,2
5	80,5	1,1
6	82,0	1,0
7	82,5	1,0
8	70,0	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	67	0
7.400	0	67	-
8.400	-2	82	-
X	-2	98	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 3.1 a) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	93,0	1,2
2	94,0	1,2
3	94,0	1,2
4	92,0	1,2
5	92,0	1,1
6	91,0	1,0
7	86,0	1,0
8	73,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.800	0	80	0
4.300	0	80	-
4.800	-	80	460
5.300	-3	80	-
9.000	-3	80	920
20.000	-3	135	1.470
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 20.000	0	0	0,05

Flugzeugklasse S 3.1 b) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	93,0	1,2
2	94,0	1,2
3	94,0	1,2
4	92,0	1,2
5	92,0	1,1
6	91,0	1,0
7	86,0	1,0
8	73,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	45	0
3.200	0	90	0
7.300	0	90	-
7.800	-	90	460
8.300	-3	90	-
15.600	-3	90	920
24.600	-3	135	1.190
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 24.600	0	0	0,03

Flugzeugklasse S 3.1 a/b) - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	83,0	1,2
2	85,0	1,2
3	82,0	1,2
4	82,5	1,2
5	83,0	1,1
6	78,5	1,0
7	80,5	1,0
8	68,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	67	0
7.400	0	67	-
8.400	-2,5	82	-
X	-2,5	98	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 3.2 a) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	96,0	1,2
2	97,0	1,2
3	97,0	1,2
4	95,0	1,2
5	95,0	1,1
6	94,0	1,0
7	89,0	1,0
8	76,0	1,0

s_o=300m

(3) PF: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.900	0	80	0
4.700	0	80	-
5.200	-	80	460
5.700	- 3	80	-
10.100	- 3	80	920
21.100	- 3	135	1.525
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 21.100	0	0	0,055

Flugzeugklasse S 3.2 b) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	96,0	1,2
2	97,0	1,2
3	97,0	1,2
4	95,0	1,2
5	95,0	1,1
6	94,0	1,0
7	89,0	1,0
8	76,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	45	0
3.300	0	90	0
7.700	0	90	-
8.200	-	90	460
8.700	-3	90	-
17.100	-3	90	920
26.100	-3	135	1.190
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 26.100	0	0	0,03

Flugzeugklasse S 3.2 a/b) - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	83,0	1,2
2	85,0	1,2
3	82,0	1,2
4	82,5	1,2
5	83,0	1,1
6	78,5	1,0
7	80,5	1,0
8	68,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	67	0
7.400	0	67	-
8.400	-2,5	82	-
X	-2,5	98	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr.2.2.3.6 VBUF-DES

Flugzeugklasse S 4 a) - Ab

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	98,0	1,2
2	106,0	1,2
3	102,0	1,2
4	100,0	1,2
5	97,0	1,1
6	93,5	1,0
7	96,0	1,0
8	83,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	40	0
1.700	0	80	0
4.700	0	80	-
5.200	-	80	460
5.700	-1,5	80	-
10.400	-1,5	80	920
21.400	-1,5	135	1.250
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 21.400	0	0	0,03

Flugzeugklasse S 4 b) - Ab

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	98,0	1,2
2	106,0	1,2
3	102,0	1,2
4	100,0	1,2
5	97,0	1,1
6	93,5	1,0
7	96,0	1,0
8	83,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	45	0
2.700	0	90	0
7.600	0	90	-
8.100	-	90	460
8.600	-1,5	90	-
17.100	-1,5	90	920
26.100	-1,5	135	1.190
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 26.100	0	0	0,03

Flugzeugklasse S 4 a/b) - An

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	81,5	1,2
2	85,5	1,2
3	82,5	1,2
4	82,5	1,2
5	82,0	1,1
6	91,5	1,0
7	89,0	1,0
8	77,0	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	67	0
7.400	0	67	-
8.400	- 3,5	82	-
X	- 3,5	98	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 5.1 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	78,0	1,0
2	81,5	1,0
3	79,5	1,0
4	78,0	1,0
5	75,0	1,0
6	72,0	1,0
7	69,0	1,0
8	59,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.100	0	75	0
5.100	0	75	-
5.600	-	75	460
6.100	-1	-	-
10.400	-1	110	650
15.000	-1	135	1.000
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 15.000	0	0	0,126

Flugzeugklasse S 5.1 - An

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	65,0	1,0
2	73,0	1,0
3	71,0	1,0
4	72,0	1,0
5	69,5	1,0
6	66,5	1,0
7	67,0	1,0
8	53,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	65	0
7.400	0	65	-
X	- 1	108	ho
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr.2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr.2.2.2.3 bzw. Nr.2.2.3.6 VBUF-DES

Flugzeugklasse S 5.2 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	86,0	1,0
2	89,5	1,0
3	87,5	1,0
4	86,0	1,0
5	83,0	1,0
6	80,0	1,0
7	77,0	1,0
8	67,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.900	0	80	0
4.100	0	80	-
4.600	-	80	460
5.100	-3	-	-
9.000	-3	115	690
15.300	-3	135	1.200
σ' [m]	dZ/dσ' [dB/m]	dV/dσ'	dH/dσ'
> 15.300	0	[s^-1]	0,113

Flugzeugklasse S 5.2 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	68,0	1,0
2	76,0	1,0
3	74,0	1,0
4	75,0	1,0
5	72,5	1,0
6	69,5	1,0
7	70,0	1,0
8	56,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	70	0
7 400	0	75	-
X	-1	108	ho
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
>X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

weiter .