TY - GEN
T1 - Conceptual design of aeropropulsion engine heat exchangers part 3
T2 - 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
AU - Panda, Pratikash
AU - Kumar, Vineet
AU - Mongia, Hukam
PY - 2013
Y1 - 2013
N2 - A major challenge which emerged in developing innovative approaches for significantly reducing the aviation Greenhouse Gas (GHG) emissions was the design of a compact heat exchanger. As a part of the FAA program under US Department of Transportation Contract Number DTRT57-11-P-80083, an LP Turbine Exhaust Driven (TED-T) secondary cycle was proposed for contrail mitigation as well as an increment of 4-5% pts in overall powerplant efficiency. It was identified that a compact heat exchanger is a critical component of TED-T. In this series of papers, Paper #1 presented some of the existing advanced compact heat exchanger (HEX) technologies along with parametric analysis of a baseline configuration. A 1-D steady state code was developed for heat transfer calculations. In this paper, a similar parametric study is presented for a Printed Circuit Heat Exchanger (PCHE) operating at the proposed TED-T cycle conditions.
AB - A major challenge which emerged in developing innovative approaches for significantly reducing the aviation Greenhouse Gas (GHG) emissions was the design of a compact heat exchanger. As a part of the FAA program under US Department of Transportation Contract Number DTRT57-11-P-80083, an LP Turbine Exhaust Driven (TED-T) secondary cycle was proposed for contrail mitigation as well as an increment of 4-5% pts in overall powerplant efficiency. It was identified that a compact heat exchanger is a critical component of TED-T. In this series of papers, Paper #1 presented some of the existing advanced compact heat exchanger (HEX) technologies along with parametric analysis of a baseline configuration. A 1-D steady state code was developed for heat transfer calculations. In this paper, a similar parametric study is presented for a Printed Circuit Heat Exchanger (PCHE) operating at the proposed TED-T cycle conditions.
UR - https://www.scopus.com/pages/publications/84881442270
M3 - Conference contribution
AN - SCOPUS:84881442270
SN - 9781624101816
T3 - 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
BT - 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
Y2 - 7 January 2013 through 10 January 2013
ER -