小林 紘

Newly-developed Compound Active Jet Noise Control Technology for Rectangular Jet Flow Noise Reduction, 

VSTech 2005, The First International Symposium on Advanced Technology of Vibration and Sound, , Hiroshima, JAPAN, Paper-050660 2005年  

Newly-developed Active Noise Absorption Control Technology for High Speed Fan Noise Reduction,. 

VSTech 2005, The First International Symposium on Advanced Technology of Vibration and Sound、 Hiroshima, JAPAN Paper-050659, Hiroshima, JAPAN 2005年  

Research on New Technology for Actively-controlled Aircraft Engine Noise Reduction”, 

Asian Joint Conference on Propulsion and Power, AJCPP 2005, Kyushu-Japan. Paper-AJCPP-A2008 2005年  

Research on New Technology for Actively-controlled Aircraft Engine Noise Reduction 

Asian Joint Conference on Propulsion and Power, AJCPP 2005, held at Kyushu-Japan Paper-AJCPP-A2008 2005年  

Newly-developed Active Noise Absorption Control Technology for High Speed Fan Noise Reduction 

, VSTech 2005, The First International Symposium on Advanced Technology of Vibration and Sound held at Hiroshima, JAPAN, Paper-050659 2005年  

Newly-developed Compound Active Jet Noise Control Technology for Rectangular Jet Flow Noise Reduction 

VSTech 2005, The First International Symposium on Advanced Technology of Vibration and Sound, held at Hiroshima, JAPAN Paper-050660 2005年  

Development of Adjustable Absorption Acoustic Liner for Active Fan Noise Control, 

NAL Research Progress 2002~2003、 National Aerospace Laboratory（Pre.JAXA) NAL Research Progress 2002~2003 2003年  

Development of Adjustable Absorption Acoustic Liner for Active Fan Noise Control, 

NAL Research Progress 2002~2003 issued at National Aerospace Laboratory (Pre. JAXA) NAL Research Progress 2002~2003 2003年  

Research on Active Noise Control Techniques and Systems for All Engine Noise Reduction, . 

The first International ESPR Symposium held at Tokyo, Japan, Paper No. B-6, 2002年5月  

Research on Active Noise Control Techniques and Systems for All Engine Noise Reduction 

The first International ESPR Symposium held at Tokyo, Japan, No. B-6 2002年5月  

Active Control of Spinning Mode with Piezoelectoric Devices 

7th International Congress on Sound and Vibration, Germany, July,2000  

Experiment to Reduce Spinning Tone Noise Issued from a Ducted Fan Using Secondary Sound Source 

Bulletin of GTSJ (1997)  

Modal Technique for Active Control of Tones Radiated from a Ducted Fan 

Journal of aircraft, 35-5 (1998), 754  

Development of an Acoustic System for Generating and Measuring Arbitrary Spinning Mode in a Duct 

Trans JSME, B-63 (1997) 614  

Variation of Supersonic Jet Noise Characteristics in Different Aspect Ratio of Rectangular Exit Nozzles 

Inter/Noise94, Vol.1, pp.499-502 (1994)  

Underexpanded Supersonic jet Noise Reduction by Combination of Tab and Ejector 

Inter/Noise94, Vol.1, pp.503-506 (1994)  

Supersonic Jet Noise Reduction Performance and Noise Reduction Mechanism of Tab Jet Noise Suppressor, 1994, The ASME International Mechanical Engineering Congress and Exposition 

The Symposium Volume on Acoustic Reduction and Wave Propagation, NCA-Vol.17, pp.149-163, (1994)  

Experimental Investigation of Unsteady Flowfield in a Supersonic Cascade Oscillating in Bending Mode, The 1994 ASME International Mechanical Engineering Congress and Exposition 

Proc. Of The Symposium on Unsteady Flows in Aeropropulsion, AD-Vol.40, pp.47-60, (1994)  

Effects of Tab Size on Supersonic Underexpanded Cold and Heated Jet Noise Suppression and Jet Thrust Loss 

15th AIAA Aereacoustic Conference, 1993, AIAA PAPER, AIAA-93-4348  

アクティブ・ノイズ･コントロールによるファン・送風等の低騒音化の研究 

平成8年度及び平成9年度国立機関公害防止等試験研究環境保全成果報告書 (1997，1998)