Visualisation of underexpanded jet flowfields in the presence of an intrusive tab

[1] André B(2013)Broadband shock-associated noise in screeching and non-screeching underexpanded supersonic jets AIAA J 51 665-673

[2] Castelain T(2013)Effect of a tab on the aerodynamical development and noise of an underexpanded supersonic jet Comptes Rendus Mécanique 341 659-666

[3] Bailly C(1999)Near exit plane effects caused by primary and primary-plus-secondary tabs AIAA J 37 192-201

[4] André B(1974)The distortion of a jet by tabs J Fluid Mech 70 801-813

[5] Castelain T(1962)Tones from a choked axisymmetric jet. ii. the self-excited loop and mode of oscillation Acustica 12 267-277

[6] Bailly C(2014)Coherent structure and sound production in the helical mode of a screeching axisymmetric jet J Fluid Mech 748 822-847

[7] Bohl D(2010)A multi-mode screech frequency prediction formula for circular supersonic jets J Acoust Soc Am 127 1251-1257

[8] Foss JF(2012)The visualization of the acoustic feedback loop in impinging underexpanded supersonic jet flows using ultra-high frame rate schlieren J Visual 15 333-341

[9] Bradbury LJS(2013)Near-field structure of underexpanded elliptic jets Exp Fluids 54 1-13

[10] Khadem A(1976)The structure of jets from notched nozzles J Fluid Mech 74 515-528

[1] André B(2013)Broadband shock-associated noise in screeching and non-screeching underexpanded supersonic jets AIAA J 51 665-673

[2] Castelain T(2013)Effect of a tab on the aerodynamical development and noise of an underexpanded supersonic jet Comptes Rendus Mécanique 341 659-666

[3] Bailly C(1999)Near exit plane effects caused by primary and primary-plus-secondary tabs AIAA J 37 192-201

[4] André B(1974)The distortion of a jet by tabs J Fluid Mech 70 801-813

[5] Castelain T(1962)Tones from a choked axisymmetric jet. ii. the self-excited loop and mode of oscillation Acustica 12 267-277

[6] Bailly C(2014)Coherent structure and sound production in the helical mode of a screeching axisymmetric jet J Fluid Mech 748 822-847

[7] Bohl D(2010)A multi-mode screech frequency prediction formula for circular supersonic jets J Acoust Soc Am 127 1251-1257

[8] Foss JF(2012)The visualization of the acoustic feedback loop in impinging underexpanded supersonic jet flows using ultra-high frame rate schlieren J Visual 15 333-341

[9] Bradbury LJS(2013)Near-field structure of underexpanded elliptic jets Exp Fluids 54 1-13

[10] Khadem A(1976)The structure of jets from notched nozzles J Fluid Mech 74 515-528