7Bartolotta P A, Shafer D G . High speed turbines : De-velopment of a turbine accelerator ( RTA ) for space ac- cess . AIAA 2003-6943.
8Snyder L E, Escher D W, DeFrancesco R L, et al. Tur- bine based combination cycle (TBCC) propulsion subsys- tem integration. AIAA 2004-3649.
9Eric J Gamble, Dan Haid, Sal D' Alessandro, et al . Du- al-mode scramjet performance model for TBCC simula- tion. AIAA 2009-5298.
10Thomas J Stueber, Daniel R Vrnak, Dzu K Le, et al. Control activity in support of NASA turbine based com- bined cycle (TBCC) research. NASA/TM-2010-216109.
二级参考文献21
1[1]U Hueter,C R.McClinton.NASA's advanced space transportation hypersonic program.AIAA-2002 -5175.
2[2]R J Shaw,L W Koops,R Hines.Progress toward meeting the propulsion technology challenges for the high speed civil transport.ISABE 99 -7005.
3[3]H Miyagi,et al.Combined cycle engine research in japanese HYPR program.AIAA-98-3278.
4[4]P A Bartolotta,D G Shafer.High speed turbines:development of a turbine accelerator (RTA) for space access.AIAA 2003-6943.
5[5]D G Shafer,N B Manelis.Development of a ground based mach 4 + revolutionary turbine accelerator technolgy demonstrator.ISABE 2003-1125.
6[6]W J D Escher.A U.S.history of airbreathing/rocket combined cycle (RBCC) propulsion for powering future aerospace transports,with a look ahead to the year 2020.ISABE99-7028.
9Shafer D G,McNelis N B.Development of a ground based mach 4 +revolutionary turbine accelerator technology demonstrator (RTATD)for access to space[R].ISABE-2003-1125,2003
10Itahara H,Nakata Y,Kimura T.Research and development of hypr90-t variable cycle tuebo engine for hst[R].ISABE-97-7013,1997