Effect of external acoustic excitation on NACA0015 discrete tonal noise
The purpose of this work is to investigate the effect of external acoustic excitation on the discrete tonal noise generated by laminar boundary layer instability. Experimental testing inside anechoic wind tunnel was done on NACA0015 in order to measure the sound spectrum at low Reynolds number of...
| Main Authors: | Andan, Amelda Dianne, Lee, Duck-Joo |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Elsevier Ltd.
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/69945/ http://irep.iium.edu.my/69945/1/%5B2018%5DEffect%20of%20external%20acoustic%20excitation%20on%20NACA0015%20discrete%20tonal%20noise.pdf http://irep.iium.edu.my/69945/7/69945_Effect%20of%20external%20acoustic%20excitation_SCOPUS.pdf |
Similar Items
Discrete tonal noise of NACA0015 airfoil at low reynolds
number
by: Andan, Amelda Dianne, et al.
Published: (2019)
by: Andan, Amelda Dianne, et al.
Published: (2019)
Estimation of aerodynamic parameters of IIUM hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)
by: Andan, Amelda Dianne, et al.
Published: (2011)
Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012)
by: Andan, Amelda Dianne, et al.
Published: (2012)
Induced rolling moment for NACA4412 plain and flapped wing
by: Elsayed, Omer Ali, et al.
Published: (2010)
by: Elsayed, Omer Ali, et al.
Published: (2010)
Evolution of NACA23012 wake vortices structure using PIV
by: Elsayed, Omer Ali, et al.
Published: (2012)
by: Elsayed, Omer Ali, et al.
Published: (2012)
CFD analysis of NACA4415 airfoil with γ−Reθ model considering natural transition
by: Islam, Mazharul, et al.
Published: (2015)
by: Islam, Mazharul, et al.
Published: (2015)
Development of the IIUM hybrid airship
by: Ping, Julian T.K., et al.
Published: (2010)
by: Ping, Julian T.K., et al.
Published: (2010)
Vortex formation in unsteady flow over NACA 4412 and NACA 4424 airfoils
by: Hadi, Muhammad Irfan, et al.
Published: (2020)
by: Hadi, Muhammad Irfan, et al.
Published: (2020)
Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
by: Asrar, Waqar, et al.
Published: (2015)
by: Asrar, Waqar, et al.
Published: (2015)
Comparative study of turbulent incompressible flow past naca airfoils
by: Abdullah, Aslam, et al.
Published: (2018)
by: Abdullah, Aslam, et al.
Published: (2018)
Numerical study of wind-tunnel wall effects on lift and drag characteristics of NACA 0012 airfoil
by: Abobaker, Mostafa, et al.
Published: (2020)
by: Abobaker, Mostafa, et al.
Published: (2020)
Effects of bio-inspired surface roughness on a swept back tapered NACA 4412 wing
by: Malik, Khurshid, et al.
Published: (2019)
by: Malik, Khurshid, et al.
Published: (2019)
Flutter analysis of supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2013)
by: Abdullah, Nur Azam, et al.
Published: (2013)
Aeroelastic tailoring of oscillating supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)
by: Abdullah, Nur Azam, et al.
Published: (2014)
Aeroelastic flutter analysis of supersonic wing with multiple external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)
by: Abdullah, Nur Azam, et al.
Published: (2014)
Investigation of base pressure variations in internal and
external suddenly expanded flows using CFD analysis
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
Aeroelastic passive control optimization of supersonic composite wing with external stores
by: Sulaeman, Erwin, et al.
Published: (2017)
by: Sulaeman, Erwin, et al.
Published: (2017)
Aerodynamics of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)
by: Andan, Amelda Dianne, et al.
Published: (2011)
Numerical investigation of the flow over delta wing and reverse delta wing
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
Investigation on flow visualization of beetle mimicking ornithopter
by: Legowo, Ari, et al.
Published: (2014)
by: Legowo, Ari, et al.
Published: (2014)
Control of base flows with micro jets
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)
by: Khan, Sher Afghan, et al.
Published: (2003)
Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)
by: Khan, Sher Afghan, et al.
Published: (2004)
Active control of base pressure in supersonic regime
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Establishing the analytical relationships for mass and volumetric mass fractions for hybrid boyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Half model testing for canard of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Active control of suddenly expanded flow from under expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)
by: Khan, Sher Afghan, et al.
Published: (2004)
Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Static longitudinal stability of a hybrid airship
by: ul-Haque, Anwar, et al.
Published: (2014)
by: ul-Haque, Anwar, et al.
Published: (2014)
Approximate function for unsteady aerodynamic kernel function of aeroelastic lifting surfaces
by: Sulaeman, Erwin, et al.
Published: (2014)
by: Sulaeman, Erwin, et al.
Published: (2014)
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Numerical study of effect of spoiler configuration on
wake vortex alleviation
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
Ant colony based model prediction of a twin rotor system
by: Toha, Siti Fauziah, et al.
Published: (2012)
by: Toha, Siti Fauziah, et al.
Published: (2012)
A review on aerodynamics of nonflapping bird wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)
Power-off static stability analysis of a clean configuration of a hybrid buoyant aircraft
by: Ul Haque, Anwar, et al.
Published: (2015)
by: Ul Haque, Anwar, et al.
Published: (2015)
Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, et al.
Published: (2018)
by: Malik, Khurshid, et al.
Published: (2018)
Quadrotor trajectory tracking using PID cascade control
by: Idres, Moumen, et al.
Published: (2017)
by: Idres, Moumen, et al.
Published: (2017)
Pulse detonation assessment for alternative fuels
by: Azami, Muhammad Hanafi, et al.
Published: (2017)
by: Azami, Muhammad Hanafi, et al.
Published: (2017)
Experimental investigation of a new spiral wingtip
by: Siddiqui, Naseeb, et al.
Published: (2018)
by: Siddiqui, Naseeb, et al.
Published: (2018)
CFD analysis of a SD 7003 airfoil with a local correlation based transition and turbulence model
by: Islam, Mazharul, et al.
Published: (2017)
by: Islam, Mazharul, et al.
Published: (2017)
Similar Items
-
Discrete tonal noise of NACA0015 airfoil at low reynolds
number
by: Andan, Amelda Dianne, et al.
Published: (2019) -
Estimation of aerodynamic parameters of IIUM hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011) -
Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012) -
Induced rolling moment for NACA4412 plain and flapped wing
by: Elsayed, Omer Ali, et al.
Published: (2010) -
Evolution of NACA23012 wake vortices structure using PIV
by: Elsayed, Omer Ali, et al.
Published: (2012)