共 50 条
- [1] EXPANDED OPERATIONAL CAPABILITIES FO THE LANGLEY MACH 7 SCRAMJET TEST FACILITY. NASA Technical Paper, 1983,
- [2] LANGLEY FACILITY FOR TESTS AT MACH 7 OF SUBSCALE, HYDROGEN-BURNING, AIRFRAME-INTEGRATABLE, SCRAMJET MODELS. Journal of Aircraft, 1976, 13 (02): : 67 - 68
- [5] Design and performance investigation of sidewall compression scramjet inlets operating from Mach 4 to Mach 7 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2011, 26 (06): : 1201 - 1208
- [6] DESIGN, TESTS, AND VERIFICATION OF A DIFFUSER SYSTEM FOR A MACH-4 SCRAMJET TEST FACILITY JOURNAL OF AIRCRAFT, 1979, 16 (10): : 641 - 642
- [9] STUDY FOR STARTING CHARACTERISTICS OF SCRAMJET ENGINE TEST FACILITY (SETF) INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION - 2012, VOL 1: ADVANCES IN AEROSPACE TECHNOLOGY, 2013, : 491 - 498
- [10] Design of Hypersonic Scramjet Engine Operating between Mach 5 to Mach 9 2019 SIXTH INTERNATIONAL CONFERENCE ON AEROSPACE SCIENCE AND ENGINEERING (ICASE), 2019, : 15 - 20