1 |
George P. Sutton, “Rocket Propulsion Element : An introduction to the engineering of Rockets”, John Wiley & Sons, Inc., pp. 365-415, 1992.
|
2 |
Michel A. Saad, Compressible fluid flow, Prentice-Hall, Inc., pp. 83-131, 1985.
|
3 |
노오현, “점성유동이론”, 박영사, pp. 201-240, 2006.
|
4 |
Dean R. Chapman, Donald M. Keuhn and Howard K. Larson,"Investigation odseparated flows in supersonic and subsonic streams with emphasis on the effect of transition", NACA-3869, 1957.
|
5 |
Charles T. Levinsky and Gerald F. Kobalter, "Feasibility demonstration of a singlechamber controllable solid rocket motor", Air Force Rocket Propulsion Lab., AFRPL-TR-67-300, 1967.
|
6 |
John Napior and Victoria Garmy, "Controllable Solid Propulsion For Launch Vehicle And Spacecraft Application", AIAA 2006-905, 2006.
|
7 |
M.J. Ostrander, J.L. Bergmans and M.E. Thomas, "Pintle Motor Challenges for Tactical Missiles", AIAA 2000-3310, 2000.
|
8 |
Christia A. Davis and Amy B. Gerards, "Variable thrust solid propulsion control using Labview", AIAA-2003-5341, 2003.
|
9 |
S.Burroughs, "Status of army pintle technology for controllable thrust propulsion", AIAA-2001-3598, 2001.
|
10 |
Francis R. Hama, "Experimental studies on the lip shock", AIAA67-29, 1967.
|
11 |
Delery, J., and Marvin. J. G., "Shock-wave boundary layer interactions", AGARD No. 280, ISBN 92-835-1519-6, 1986.
|
12 |
Barry L. Reeves, and Lester Lees,"Theory of laminar near wake of blunt bodies in hypersonic flow", AIAA journal, Vol. 3, No. 11 , pp. 2061-2074, 1965.
DOI
|
13 |
김중근, 이지형, 장홍빈, “핀틀 공압 시험 결과 보고”, 국방과학연구소 보고서, ADDR-421-080682, 2008.
|
14 |
Jan Ostlund, " Flow processing in rocket engine nozzle with focus on flow separation and side-loads", TRITA-MEK, Technical Report 2002:09, ISSN 0348-467X, 2002.
|