International Books & Journals Publisher
Menu
1(4), (2022):20-24. DOI: http://doi.org/10.46632/jame/1/4/4
Nikkisha S, Ankit Kumar Mishra
Augmentation plays a crucial role in many aircrafts and jet engines to elevate the thrust. Thrust is oe of the four fundamental forces of an aircraft. Augmentation methods are used in certain cases to increase the thrust to perform better landing and take-off. There is various augmentation methods in which afterburner is mostly used over other augmentation methods because of its advantages. In this paper an overview has been provided for thrust augmentation and its different control methods
J. Bulman and T. M. Neill, Simulated LOX-Augmented Nuclear Thermal Rocket (LANTR) Testing, AlAA 2000-3897 (1999), pp-2-5.
Scott Forde, Mel Bulman, Todd Neill, Thrust Augmentation Nozzle (TAN) Concept for Rocket Engine Booster Applications (2005). 56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, pp 1-6.
Col Timothy Lawrence, Nuclear Thermal Rocket Propulsion Systems, IAA White Paper, pp 1-16.
Bhattacharyya, S. (2011). A Rational Strategy for Nuclear Thermal Rocket Development. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, pp-1-15
David R. McCurdy, Stanley K. Borowski, Thomas W. Packard, NUCLEAR THERMAL ROCKET (NTR) PROPULSION: A PROVEN GAME-CHANGING TECHNOLOGY FOR FUTURE HUMAN EXPLORATION MISSIONS, Global Space Exploration Conference. Pp-1-15.
Borowski, S. K. (2013). Nuclear Thermal Propulsion: Past Accomplishments, Present Efforts, and a Look Ahead. Journal of Aerospace Engineering, 26(2), 334–342.
Krishnamurthy1 and A. Vignesh2, Liquid Oxygen Augmented Gas Core Nuclear Thermal Rocket, Advances in Aerospace Science and Applications. ISSN 2277-3223 Volume 3, Number 3 (2013), pp. 239-244.
Belair, M. L., Sarmiento, C., & Lavelle, T. (2013). Nuclear Thermal Rocket Simulation in NPSS. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.pp-1-15.
John Bucknell, The Nuclear Thermal Turbo Rocket – A Conceptual High-Performance Earth-orbit Propulsion System, Propulsion and Energy Forum, July 27-29, 2015, Orlando, FL, 51st AIAA/SAE/ASEE Joint Propulsion Conference.pp-1-20.
Seung Hyung Nam, Paolo Venneri, Yonghee Kim, JeongIk Lee, Soon Heung Chang, and Yong HoonJeong, Innovative Concept For An Ultra Small Nuclear Thermal Rocket Utilizing a New Moderator Reactor, Nam, S. H., Venneri, P., Kim, Y., Lee, J. I., Chang, S. H., &Jeong, Y. H. (2015). Innovative concept for an ultra-small nuclear thermal rocket utilizing a new moderated reactor. Nuclear Engineering and Technology, 47(6), 678–699.
Arias, F. J. (2016). On the Use of a Pulsed Nuclear Thermal Rocket for Interplanetary Travel. 52nd AIAA/SAE/ASEE Joint Propulsion Conference,pp-1-9.
Paolo Venneri, Yonghee Kim, Advancements in the Development of Low Enriched Uranium Nuclear Thermal Rockets, 5th International Symposium on Innovative Nuclear Energy Systems, pp-1-8.
Steiling (1975), An Investigation of the Static Thrust Augmentation Capabilities of a Divergent Ejector-Afterburner, pp1-115.
GREEN, C. J., & MC CULLOUGH, F. (1963). LIQUID INJECTION THRUST VECTOR CONTROL. AIAA Journal, 1(3), 573–578.
Hugh M (1961), A Thermodynamic Analysis of Thrust Augmentation for Nuclear Rockets,NASA, 1-30.
Alperin, M., & Wu, J.-J. (1983). Thrust Augmenting Ejectors, Part I. AIAA Journal, 21(10), 1428–1436.
Fleming W A,Experimental Investigation of Tail-pipe-burner Design Variables,NACA.
Bevilaqua, P. M. (1974). Evaluation of Hypermixing for Thrust Augmenting Ejectors. Journal of Aircraft, 11(6), 348–354.
Presz, Jr., W., Reynolds, G., & McCormick, D. (1994). Thrust augmentation using mixer-ejector-diffuser systems.
Quinn, B. (1973). Compact Ejector Thrust Augmentation. Journal of Aircraft, 10(8), 481–486.
Bevilaqua, P. M. (1978). Lifting Surface Theory for Thrust-Augmenting Ejectors. AIAA Journal, 16(5), 475–481.
Davis, R., Bulman, M., & Yam, C. (2006). Numerical Simulation of a Thrust Augmented Rocket Nozzle. 42nd AIAA/ASME/SAE/ASEE. 1-10
Dotan Rami (1978),Turbojet Thrust Augmentation by Sudden Expansion Type Afterburner, 1-58.
https://engineering.purdue.edu/AAE/research/propulsion/Info/jets/basics/afterburner
EE Zukoski (1978),AfterBurners, 47-50.
Lovett, J., Brogan, T., Philippona, D., Kiel, B., & Thompson, T. (2004). Development Needs for Advanced Afterburner Designs, 1-12.
Rogers, D. E. (1956). A Mechanism for High-Frequency Oscillation in Ramjet Combustors and Afterburners. Journal of Jet Propulsion, 26(6), 456–462.
Clinton Wilcox (1951),ANALYSLS OF THRUST AUGMENTATION OF TURBOJET ENGINES BY WATER INJECTION AT COMPRESSOR INLET ll?CXIIDING CHARTS FOR CALCULATING COMPRESS1ON PROCESSES WITH WATER INJECTION , NACA, 97-116.
David L.Daggett (2004), Revisiting Water Injection For Commercial Aircraft. 01-3108.
Zhu, S., Hu, B., Akehurst, S., Copeland, C., Lewis, A., Yuan, H., … Branney, C. (2019). A review of water injection applied on the internal combustion engine. Energy Conversion and Management, 184, 139–158.
ROWE, M. R., & LADD, G. T. (1946). WATER INJECTION for Aircraft Engines. SAE Transactions, 54, 26–44.
Boretti, A. (2011). Stoichiometric H2ICEs with water injection. International Journal of Hydrogen Energy, 36(7), 4469–4473.
MACA staff members (1940), Turbojet engine thrust augmentation research.
MiroslawKowalski,THE ADVANTAGES OF USING A BLEED OF AIR FROM BEHIND THE COMPRESSOR AND SUPPLYING IT BEHIND THE TURBINE IN AN AIRCRAFT ENGINE, 381-394.
Alison B Evans (1991), The effects of compressor seventh stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine.
Rios, H., González, E., Rodriguez, C., Siller, H. R., &Contero, M. (2013). A Mobile Solution to Enhance Training and Execution of Troubleshooting Techniques of the Engine Air Bleed System on Boeing 737. Procedia Computer Science, 25, 161–170.
Peltier, V., Dullenkopf, K., & Bauer, H.-J. (2012). Experimental Investigation of the Performance of Different Bleed Air System Designs. Volume 8: Turbomachinery, Parts A, B, and C.
Slingerland, R., & Zandstra, S. (2007). Bleed Air versus Electric Power Off-takes from a Turbofan Gas Turbine over the Flight Cycle. 1-12.
Wu, X., Singh, S., Choi, J., & Chahine, G.L. (2012). Waterjet Thrust Augmentation using High Void Fraction Air Injection.
Nikkisha S, Ankit Kumar Mishra, “Thrust Augmentation and its Control Methods: Short Overview”, REST Journal on Advances in Mechanical Engineering, 1(4), (2022):20-24.