Acoustic Experiments for Special Forces Helicopter Operations

For military missions, the helicopter is a versatile aircraft with many benefits. However, the high levels of noise radiation enable large acoustic detection ranges. For mission success, knowledge of acoustic radiation and propagation is paramount. This paper describes the results of acoustic measurements for a helicopter that is typically used for operations by the German special forces. The measurements include identification of the global noise radiation during different flight conditions, determination of the time between acoustic detection and arrival at the target location, and determination of the acoustic detection distance. Different approaches and departure procedures were executed, and the acoustic radiation was measured. Results indicate that during approaches, the most noise is generated either during the transition from steady level flight to descent/deceleration or at the end of the flare procedure. For the helicopter considered here, a left turn departure generates more noise at a target location then a right turn departure.

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Publication Details

Journal
Aerospace
Published
2025-10-08
DOI
https://doi.org/10.3390/aerospace12100903
Primary Topic
Acoustic Wave Phenomena Research
Type
article
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article

Acoustic Experiments for Special Forces Helicopter Operations

W.F.J. Olsman
Aerospace
Acoustic Wave Phenomena Research
article

Acoustic Experiments for Special Forces Helicopter Operations

W.F.J. Olsman
article en

Abstract

For military missions, the helicopter is a versatile aircraft with many benefits. However, the high levels of noise radiation enable large acoustic detection ranges. For mission success, knowledge of acoustic radiation and propagation is paramount. This paper describes the results of acoustic measurements for a helicopter that is typically used for operations by the German special forces. The measurements include identification of the global noise radiation during different flight conditions, determination of the time between acoustic detection and arrival at the target location, and determination of the acoustic detection distance. Different approaches and departure procedures were executed, and the acoustic radiation was measured. Results indicate that during approaches, the most noise is generated either during the transition from steady level flight to descent/deceleration or at the end of the flare procedure. For the helicopter considered here, a left turn departure generates more noise at a target location then a right turn departure.

AerospaceVol. 12(10)
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR) (DE)
Openalex Percentile: Top 73%
Acoustic Wave Phenomena Research
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Acoustic Experiments for Special Forces Helicopter Operations — W.F.J. Olsman · Aerospace (2025) | TGRS Research Map | TGRS