المؤلفون: Yin, Jianping, Rossignol, Karl-Stephane, Rottmann, Lukas, Schwarz, Thorsten

مصطلحات موضوعية: Acoustic Wind Tunnel, acoustic analogy, Unsteady Panel Method, SMALL-SCALE ROTOR CONFIGURATIONS, Helicopter Acoustics, CFD, Urban Air Mobility (UAM)

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::1d939d5cab13aac78772cd7fd3ebc44e
https://elib.dlr.de/190347/

المؤلفون: Yin J., Rossignol K. S., Reboul G., Mortain F., Vigevano L., Zanotti A., Gibertini G., Barbarino M., Testa C., Bernardini G., Brouwer H.

المساهمون: Yin, J., Rossignol, K. S., Reboul, G., Mortain, F., Vigevano, L., Zanotti, A., Gibertini, G., Barbarino, M., Testa, C., Bernardini, G., Brouwer, H.

مصطلحات موضوعية: Acoustic Wind Tunnel, BEM, scattering test, noise Propagation, Helicopter Acoustics, Rotorcraft Fuselage Scattering, Computational Aero-Acoustiacoustic, shielding experiments, GARTEUR

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::eae6c051c67dfd36e416891a006766ae
http://hdl.handle.net/11311/1184737

المؤلفون: Yin, Jianping, Rossignol, Karl-Stephane

مصطلحات موضوعية: Boundary Element Method, Installation Effects, noise Propagation, Helicopter Acoustics, Rotorcraft Fuselage Scattering, Computational Aeroacoustic, GARTEUR

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::3c92a5806f2f52e0e3b4cee51519fdb8
https://doi.org/10.1016/j.jsv.2020.115540

المؤلفون: Jianping Yin

مصطلحات موضوعية: Physics::Instrumentation and Detectors, Acoustics, Installation Effects, Aerospace Engineering, Helicopter Acoustics, Rotorcraft Fuselage Scattering, 02 engineering and technology, 01 natural sciences, 010305 fluids & plasmas, law.invention, 0203 mechanical engineering, law, 0103 physical sciences, Computational Aeroacoustic, Boundary element method, Physics, 020301 aerospace & aeronautics, Ffowcs Williams–Hawkings (FW-H), Rotor (electric), Boundary Element Method, noise Propagation, Forward flight, Noise, Fuselage, free-wake unsteady panel method, Electromagnetic shielding, Helicopter rotor, Multipole expansion

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cbacf74fafdff776c14b6f352f3ec973
https://elib.dlr.de/128674/

المؤلفون: Giovanni Bernardini, Jacopo Serafini, Karl-Stéphane Rossignol, Massimo Gennaretti, D. Bianco, Gabriel Reboul, Caterina Poggi, Luigi Vigevano, Stevie Ray Janssen, H. Brouwer, Jianping Yin, Claudio Testa, Mattia Barbarino

المساهمون: Laboratory of Information, Network and Communication Sciences (LINCS), Université Pierre et Marie Curie - Paris 6 (UPMC)-Institut National de Recherche en Informatique et en Automatique (Inria)-Institut Mines-Télécom [Paris] (IMT), DAAA, ONERA, Université Paris-Saclay (COmUE) [Châtillon], ONERA-Université Paris Saclay (COmUE), Politecnico di Milano [Milan] (POLIMI), Department of Molecular Medicine, Institut Pasteur, Fondation Cenci Bolognetti - Istituto Pasteur Italia, Fondazione Cenci Bolognetti, Réseau International des Instituts Pasteur (RIIP)-Réseau International des Instituts Pasteur (RIIP)-Università degli Studi di Roma 'La Sapienza' = Sapienza University [Rome] (UNIROMA), Yin, J., Rossignol, K. S., Barbarino, M., Bianco, D., Testa, C., Brouwer, H., Janssen, S. R., Reboul, G., Vigevano, L., Bernardini, G., Gennaretti, M., Serafini, J., Poggi, C., Institut Mines-Télécom [Paris] (IMT)-Institut National de Recherche en Informatique et en Automatique (Inria)-Université Pierre et Marie Curie - Paris 6 (UPMC), Réseau International des Instituts Pasteur (RIIP)-Réseau International des Instituts Pasteur (RIIP)-Università degli Studi di Roma 'La Sapienza' = Sapienza University [Rome]

المصدر: CEAS Aeronautical Journal
CEAS Aeronautical Journal, 2018, 10 (2), pp.531-551. ⟨10.1007/s13272-018-0333-0⟩
CEAS Aeronautical Journal, Springer, 2018, 10 (2), pp.531-551. ⟨10.1007/s13272-018-0333-0⟩

مصطلحات موضوعية: SAILING VESSELS, Helmholtz equation, Computer science, Acoustics, Aerospace Engineering, Transportation, Helicopter Acoustics, Rotorcraft Fuselage Scattering, 02 engineering and technology, 01 natural sciences, Wind speed, 010305 fluids & plasmas, Computational Aero-Acoustiacoustic, symbols.namesake, COMPUTATIONAL AEROACOUSTICS, [SPI]Engineering Sciences [physics], 0203 mechanical engineering, FORECASTING, 0103 physical sciences, BOUNDARY ELEMENT METHOD, spheres, NUMERICAL METHODS, Boundary element method, Wind tunnel, shielding experiments, DLR Acoustic Wind Tunnel, GARTEUR, [PHYS]Physics [physics], 020301 aerospace & aeronautics, Numerical analysis, scattering test, noise Propagation, Euler equations, [PHYS.MECA.ACOU]Physics [physics]/Mechanics [physics]/Acoustics [physics.class-ph], COMPUTATIONAL FLUID DYNAMICS, analytical solution, Noise, DLR Laser generated Sound, Fuselage, symbols, WIND TUNNELS

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d0b5fd417a4dc762d64b555157258623
http://hdl.handle.net/11311/1079517

المؤلفون: Yin, Jianping, Zanotti, Alex, Rossignol, Karl-Stephane, Gibertini, G., Vigevano, Luigi

مصطلحات موضوعية: analytical solution, DLR Laser generated Sound, scattering test, noise Propagation, Helicopter Acoustics, Rotorcraft Fuselage Scattering, spheres, Computational Aero-Acoustiacoustic, shielding experiments, DLR Acoustic Wind Tunnel, GARTEUR

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a9d03ecccfc5cf12f5dc7c4f79ee50db
http://hdl.handle.net/11311/1065457

المؤلفون: Barbarino, M., Bianco, D., Yin, J., Lummer, M., Reboul, G., Gennaretti, M., Bernardini, G., Claudio Testa

المساهمون: European Rotorcraft Forum, Barbarino, M., Bianco, D., Yin, J., Lummer, M., Reboul, G., Gennaretti, Massimo, Bernardini, Giovanni, Testa, Claudio

المصدر: Scopus-Elsevier

مصطلحات موضوعية: Boundary Element Method, noise Propagation, Computational Aero-Acoustics, Helicopter Acoustics, Rotorcraft Fuselage Scattering, GARTEUR

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::0b938295ecb3203ca81858c99d90df08
https://elib.dlr.de/108071/

المؤلفون: Olsman, W.F.J.

مصطلحات موضوعية: Helicopter acoustics

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::08b86c0141be4320e003cb4d4d761a9e
https://elib.dlr.de/99916/

المؤلفون: Yin, Jianping, van der Wall, Berend G., Wilke, Gunther

مصطلحات موضوعية: Blade vortex interaction (BVI) noise, Free wake, Main rotor and Tail rotor interaction, Helicopter Acoustics, elastic deformation, Main rotor/Tail Rotor/Fuselage mutual interaction, Sound propagation, Panel method

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::02ffd83f055083fa30f01130480a9304
https://elib.dlr.de/90754/

المؤلفون: Yin, Jianping

مصطلحات موضوعية: Blade vortex interaction (BVI) noise, Free wake, Main rotor and Tail rotor interaction, Helicopter Acoustics, Main rotor/Tail Rotor/Fuselage mutual interaction, Sound propagation, Panel method

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::282b7391049ed6edadc5e05dbe99276e
https://elib.dlr.de/77907/

المؤلفون: Greenwood, Eric

المساهمون: Schmitz, Fredric H, Digital Repository at the University of Maryland, University of Maryland (College Park, Md.), Aerospace Engineering

مصطلحات موضوعية: Engineering, Aerospace, acoustic flight testing, blade vortex interaction, ground noise contour, helicopter acoustics, rotorcraft acoustics, rotorcraft noise model

وصف الملف: 8394677 bytes; application/pdf

Relation: http://hdl.handle.net/1903/8983

الاتاحة: http://hdl.handle.net/1903/8983

المؤلفون: Koushik, Sudarshan

المساهمون: Schmitz, Fredric H, Digital Repository at the University of Maryland, University of Maryland (College Park, Md.), Aerospace Engineering

مصطلحات موضوعية: Engineering, Aerospace, Helicopter acoustics, blade-vortex interaction, noise measurement, BVI

وصف الملف: 4641936 bytes; application/pdf

Relation: http://hdl.handle.net/1903/7620

الاتاحة: http://hdl.handle.net/1903/7620

المؤلفون: Yin, J., Rossignol, K. -S, Barbarino, M., Bianco, D., Testa, C., Brouwer, H., Janssen, S. R., Reboul, G., Vigevano, L., Bernardini, G., Massimo Gennaretti, Serafini, J., Poggi, C.

المساهمون: Yin, J., Rossignol, K. S., Barbarino, M., Bianco, D., Testa, C., Brouwer, H., Janssen, S. R., Reboul, G., Vigevano, L., Bernardini, Giovanni, Gennaretti, Massimo, Serafini, Jacopo, Poggi, Caterina

المصدر: Scopus-Elsevier

مصطلحات موضوعية: analytical solution, DLR Laser generated Sound, scattering test, noise Propagation, Helicopter Acoustics, Rotorcraft Fuselage Scattering, spheres, Computational Aero-Acoustiacoustic, shielding experiments, DLR Acoustic Wind Tunnel, GARTEUR

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::2e9673eee0aedbfde5f8f92d4b47333a
http://www.scopus.com/inward/record.url?eid=2-s2.0-85054345923&partnerID=MN8TOARS