Ignition Delay Times of Jet-A/Air Mixtures
Zhukov, V. and Starikovskiy, A. and Sechenov, V. (2012) Ignition Delay Times of Jet-A/Air Mixtures. In: Proceedings (AIAA-2012-501). 50th AIAA Aerospace Sciences Meeting, 9. - 12. Jan. 2012, Nashville, TN, USA.
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Ignition of Jet-A/air mixtures was studied behind reflected shock waves. Heating of shock tube at temperature of 150 °C was used to prepare a homogeneous fuel mixture. Ignition delay times were measured from OH emission at 309 nm (A2Σ – X2Π) and from absorption of He-Ne laser radiation at 3.3922 μm. The conditions behind shock waves were calculated by one-dimensional shock wave theory from initial conditions T1, P1, mixture composition and incident shock wave velocity. The ignition delay times were obtained at two fixed pressures 10, 20 atm for lean, stoichiometric and rich mixtures (ø=0.5, 1, 2) at an overall temperature range of 1040-1380 K.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Ignition Delay Times of Jet-A/Air Mixtures|
|Journal or Publication Title:||Proceedings|
|In ISI Web of Science:||No|
|Event Title:||50th AIAA Aerospace Sciences Meeting|
|Event Location:||Nashville, TN, USA|
|Event Type:||international Conference|
|Event Dates:||9. - 12. Jan. 2012|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Raumfahrt|
|HGF - Program Themes:||R RP - Raumtransport|
|DLR - Research area:||Raumfahrt|
|DLR - Program:||R RP - Raumtransport|
|DLR - Research theme (Project):||R - Antriebsystemtechnik - Raketenantriebtests|
|Institutes and Institutions:||Institute of Space Propulsion > Raketenantriebe|
|Deposited By:||Michaela Hanke|
|Deposited On:||28 Nov 2012 12:33|
|Last Modified:||28 Nov 2012 12:33|
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