- CadnaA.
- Why CadnaA?.
- Modeling and Calculation.
- Features.
- Extensions.
- BMP - Bitmap Handling.
- BPL - Backtracing of Sound Power Levels.
- SET - Sound Emission and Transmission.
- XL - Strategic Noise Mapping.
- FLG - Aircraft Noise.
- ICAN Calculation Method.
- AzB Calculation Method.
- ECAC Calculation Method.
- DIN Calculation Method.
- APL - Air Pollutants.
- 64 - CadnaA 64-bit Version.
- CALC - Networked Calculation.
- CadnaSAK.
- BASTIAN.
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Out now! CadnaA 4.2

CadnaA version 4.2 includes several new features and is available now.
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CadnaA Webtutorial
Teach yourself the elements of CadnaA with the CadnaA Webtutorial.
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CadnaA Users
CadnaA is successfully applied in many different industries in more than 60 countries all over the world.
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Success Stories
Noise Mapping Austria
The strategic noise maps for all of Austria were calculated with CadnaA.
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Air Pollution Calculation
CadnaA with Option APL allows calculation, assessment and presentation of air pollutant distribution.
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View typical applications
Calculation according to AzB Method
The calculation is based on the guideline AzB "Guidance for the calculation of noise protection areas at civil and military airports according to the German act on aircraft noise (Fluglärmgesetz, dated 30 March 1971)". There the calculation of the energy-equivalent sound pressure level Leq is based on the model that the highest sound level L and noise duration t are only dependent on the flight and acoustic data that is characteristic for each aircraft as well as the distance s, the angular height alpha and the arc length sigma (see fig. b: section along line P-U).
The distance s is the distance of the aircraft from the immission point P when flying over point U. The angular height alpha is the angle which - on flying over point U - includes the straight-line connection of the aircraft and the immission point P with the reference plane. The arc length sigma is the distance between the foot F of the perpendicular dropped on the flight route from immission point P and the runway reference point PB, measured along the flight route (see fig. a: projection onto reference plane).
With growing distance s, the sound level L decreases while the noise duration t increases. If the angular height alpha is small, the sound-absorbing ground causes a reduction in sound level L. The arc length sigma is relevant as the engine power and the flight speed can change along the flight route. With rising engine power, the sound level L increases while with rising flight speed, the noise duration t decreases.
Calculation Settings
- Parameter of half-value switchable q=4 or q=3
- Several procedures for integration of air corridor
- Free input of reference time interval
- Calculaton result: Leq (La and Lb) or Ld/Ln (separate calculation for day and night)
- Optional consideration of receiver height
- Maximum level statistics with editable level range and class width
- Calculation of the number of exceedings above a defined threshold
Related Information
Overview of Option FLG for aircraft noise calculation
Aircraft noise calculation according to ICAN (AzB 2008) with Option FLG
Aircraft noise calculation according to ECAC Doc. 29 with Option FLG
Aircraft noise calculation according to DIN 45684-1 with Option FLG
Noise mapping with CadnaA


