TY - GEN
T1 - An preliminary overview analysis on the internal waverider inlets for ramjet
AU - Zuo, Fengyuan
AU - Huang, Guoping
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Challenges and advantages of inward turning inlets for ramjet is investigated in this paper. Based on the qualitative and quantitative analysis, the inward turning inlets in ramjet field have following substantial advantages. 1) higher mass airflow capture, 2) shorter compressive length, 3) lower wetted area, 4) lower pressure drag, 5) lower skin friction drag. In detail, comparing to two-dimensional classical compression in ramjet, the total pressure recovery of ICFC inward-turning compression increases 28.0%; the compressive length decreases 5%; the wetted area decreases 15.7% and the pressure drag decreases 12.1%. In addition, the different throat Mach number between ramjet and scramjet of inward turning inlet makes the self-starting ability for ramjet facing more difficulty challenge. Furthermore, the inward turning inlets face more difficulty challenge than traditional inlets in ramjet field.
AB - Challenges and advantages of inward turning inlets for ramjet is investigated in this paper. Based on the qualitative and quantitative analysis, the inward turning inlets in ramjet field have following substantial advantages. 1) higher mass airflow capture, 2) shorter compressive length, 3) lower wetted area, 4) lower pressure drag, 5) lower skin friction drag. In detail, comparing to two-dimensional classical compression in ramjet, the total pressure recovery of ICFC inward-turning compression increases 28.0%; the compressive length decreases 5%; the wetted area decreases 15.7% and the pressure drag decreases 12.1%. In addition, the different throat Mach number between ramjet and scramjet of inward turning inlet makes the self-starting ability for ramjet facing more difficulty challenge. Furthermore, the inward turning inlets face more difficulty challenge than traditional inlets in ramjet field.
UR - https://www.scopus.com/pages/publications/85017546506
M3 - 会议稿件
AN - SCOPUS:85017546506
SN - 9781624104633
T3 - 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
BT - 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
Y2 - 6 March 2017 through 9 March 2017
ER -