• 제목/요약/키워드: Military Aircraft Noise

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군용항공기 소음평가 단위에 관한 연구 (A Study on the Evaluation Unit of a Military Aircraft Noise)

  • 이준호
    • 한국소음진동공학회논문집
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    • 제15권5호
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    • pp.550-557
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    • 2005
  • Korean 'Law of Aviation' and 'Test Method of Measuring Noise and Vibration' designate to use WECPNL metric based on $L_{max}$ measurement for the accessment of aircraft noise in Korea. However, time duration of noise event can not be considered in $L_{max}$ metric in principle, compensation on the duration has been utilized. A study was done recently to evaluate appropriate duration compensation for the accessment of military aircraft noise under current metric of WECPNL and $L_{max}$. This study was carried out to evaluate what metric is the most appropriate to express aircraft noise including time duration of single noise event, computing and comparing noise exposure with 1 second noise measurement data of military aircraft in $L_{max}$, $L_{Aeq,\;T}$ and SEL. This study shows SEL is the most appropriate noise metric for the evaluation of noise exposure with time duration such as aircraft noise without compensation. It is suggested to use SEL noise metric instead of $L_{max}$ noise metric with duration compensation for the aircraft noise accessment either military aircraft or civilian aircraft.

군용항공기의 운항 경로 변경에 따른 소음영향 및 저감 평가 (Evaluation on the Noise Influence and Reduction due to the Change of Military Aircraft Flight Path)

  • 이진영;이찬;길현권
    • 환경영향평가
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    • 제18권3호
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    • pp.143-150
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    • 2009
  • The present study investigates the effects of the flight paths of military aircraft on noise map and its WECPNL(Weighted Equivalent Continuous Perceived Noise Level) distribution. Aircraft noise modeling and simulation have been performed on a Korean military air base by means of INM(Integrated Noise Model) with the input data of airfield location, aircraft specifications, flight paths and aircraft's operation schedules. The result of noise modelling has been verified in comparison with the result of measured noise level. The flight path of military aircraft, as the key parameter of the present study, was modeled by combining takeoff, overfly, approach and touch-and-go modes. The present INM simulations have been conducted for various flight path cases with different takeoff, approach modes and overfly modes. The simulation results showed that the change of flight path can remarkably affect the noise influence region and the WECPNL distribution around the airfield.

민간항공기 소음평가 단위에 관한 연구 (A Study on the Evaluation Metric of a Civil Aircraft Noise)

  • 이준호
    • 한국소음진동공학회논문집
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    • 제16권5호
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    • pp.503-513
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    • 2006
  • The duration time of aircraft noise event is also an important factor for the evaluation of civil aircraft noise, which is considered as a notable characteristic of military aircraft noise. SEL is proved as a suitable noise metric for the measuring military aircraft noise of various flight pattern considering the duration time of noise event. This study reviews whether SEL is a suitable for measuring civil aircraft noise and study shows SEL is fairly compensating the duration time of civil aircraft noise event for the evaluation of aircraft noise. Noise metric for the evaluation aircraft noise based on SEL is more appropriate than based on $L_{MAX}$ for compensating duration time of noise event either military aircraft or civil aircraft. In this reason, current formula of WECPNL based on energy average of measured $L_{MAX}$ for the evaluation of aircraft noise impact in 'Test Method of Noise and Vibration of Korea' is recommended to be amended to formula of WECPNL based on energy average of measured SEL considering compensation of noise event duration time, if WECPNL is not based on measured EPNL, a metric compensating duration time.

군용 비행장 내 실내소음 기준 설정에 관한 연구 (Study on Establishing the Indoor Noise Standard in Military Airport)

  • 고준희;최남수;백철;조만희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.701-703
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    • 2014
  • The intense noise generated by military aircraft hans a significant impact on ground crews and their families on airbase. For minimizing the impact of the aircraft noise on the airport, appropriate indoor noise standard is required. This paper studied to establish the indoor noise standard on the military airport. The aircraft noise was measured and analyzed the frequence characteristics. the remodeling of office for the noise mitigation was enforced to verify the appropriate internal noise standard and to select the method of reinforcement. The noise standard was classified three categories according to the dwelling, office and usage of building with flight train facilities and banishment in military airfield.

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민항기와 군용기가 혼합된 공항 주변지역의 항공기 소음에 대한 거주자 반응 (Subjective Response for the Aircraft Noise in the Region around Airport mixed with Commercial and Military Aircrafts)

  • 백형배;박현구;김선우
    • KIEAE Journal
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    • 제9권1호
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    • pp.99-106
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    • 2009
  • This study aims to survey the acoustical environment in the region around airport where there are various transportation noises such as aircraft noise, railway noise and traffic noise, and to analyze the subjective response on the noise to the people who live in house or work in office nearby airport. Measurement and subjective response evaluation were carried out at the same time and outdoor noise level was measured all day long to calculate one day results such as average Leq or one day WECPNL etc. The results showed that the military aircraft produces very high level comparing with commercial aircraft, for instance the sound level of commercial outdoor was lower than that of military aircraft indoor. Double and triple window were more effective for controlling the noise than single window, which showed the possibility of sound insulation treatment by installing windows having higher sound insulation performance. Finally the subjective response was resulted that the most annoying noise is from aircraft and counterplan they hope is 'airport moving out'. Leq 65 dB(A), the criteria value of sound insulation treatment, was corresponding to the subjective response of median annoyance '4' out of 7th scale.

민간항공기와 군용항공기 소음에 의한 성가심 반응 비교 (Comparison of community annoyance from commercial and military aircraft noise)

  • 이수갑;김규태;김재환;홍지영;임창우
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 추계학술대회논문집
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    • pp.425-429
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    • 2007
  • The noise problem has been a public interest for several years in Korea. Especially, the noises which were emitted from aircrafts on the airport and in the air have injurious effects on people over a vast range. Hence, there need vast data on the aircraft noise to evaluate the effect of various parameters. In present study, the works which consist of social surveys and noise measurements were conducted at points near the airport and the airbase. Total of 1,784 participants give effective responses in forty-five areas nearby the measurement points. Questionnaires asked the responses concerned with attitude, noise sensitivity, directive effects, secondary effects, annoyance and attempts to lower noise level exposed. From the field survey, the doseresponse relationship of community response to aircraft noise was established and there are different characteristics between civil and military aircraft. Though the study is still continuing on a few interest, one among some results is that %HA (%highly annoyed) of civil aircraft is higher than military's under the 70 WECPNL.

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군용항공기의 운항 경로에 따른 WECPNL 변화에 관한 연구 (Study on the WECPNL Variation due to the Change of Military Aircraft Flight Path)

  • 이진영;이찬;길현권;황성국
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 추계학술대회논문집
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    • pp.793-795
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    • 2007
  • The present study investigates the effect of the flight path of military aircraft on noise map and its WECPNL distribution. Aircraft noise modeling and simulation are made on a Korean military airport by INM(Integrated Noise Model) 6.2 version, and the flight path of military aircraft is modeled by combining takeoff, overfly, approach and touch-and-go modes. The present INM simulations are conducted for two cases with different overfly modes and show that the change of overfly mode remarkably affects the noise influence region and the WECPNL distribution around the aircraft.

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군용항공기의 이.착륙 패턴에 따른 소음 영향 분석 (Analysis of the Noise Effects due to the Variation of Military Aircraft Flight Patterns of Takeoff and Approach)

  • 이진영;이찬;길현권
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 춘계학술대회논문집
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    • pp.626-629
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    • 2008
  • The present study investigates the effect of the flight patterns of military aircraft for takeoff and approach on noise map. Aircraft noise modeling and simulation have been made on a Korean military airport by INM(Integrated Noise Model). The flight path of a military aircraft is modeled with takeoff, overfly, approach and touch-and-go modes. The present INM simulations are conducted for various cases with change of different takeoff and approach modes. It show that the change of takeoff and approach modes can cause considerable noise effects on the noise influence region around the airport.

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광주공항 주변의 항공기 소음피해 현황과 대책 (The Present Situation of Aircraft Noise Damage and the Counterplan against Aircraft Noise in KWANGJU Airport)

  • 송병흠
    • 한국항공운항학회지
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    • 제7권1호
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    • pp.65-75
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    • 1999
  • Nowadays military aircraft noise significantly affect a number of people near military airport. This paper is mainly focused on a presentation of the proper counterplan against aircraft noise in KWANGJU airport, after research and analyze the present situation of aircraft noise damage and problems, including various civil appeal and Korean laws and policies, related to KWANGJU airport.

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군용항공기 소음예측시 오차저감에 관한 연구 (A Study on the Reduction of Simulation Errors in the Prediction of Military Aircraft Noise)

  • 김미진;이병찬
    • 한국소음진동공학회논문집
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    • 제17권3호
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    • pp.249-256
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    • 2007
  • Aircraft noise is a serious problem to inhabitants near airports. INM is one of programs for determining the predicted noise impact in the vicinity of airports. It has been widely used for engineers to evaluate aircraft noise. However it is difficult to predict aircraft noise in case of lack of exact INM input data. The exact informations about a fighter plane are not known well for a security problem. This study presents methods of reducing errors between measurement and simulation when the exact INM input data is not known. Especially we adjusted the thrust force of aircraft engine and reduced the error.