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Multi-Functional Nozzle For Advanced Weapon Systems
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English
Abstract
Over the past decade the performance requirements placed on advanced weapon systems has increased significantly. These requirements are aimed at increased operational capability and result in the necessity to improve both the component efficiencies and operational characteristics of the weapon system components. From the standpoint of the exhaust system component, the requirements for greater operational capability have placed more emphasis on both engine/airframe integration and nozzle flexibility. Design studies have shown that in order to meet the future capabilities of the advanced weapon systems, multi-functional exhaust nozzle systems with thrust reversing and thrust vectoring capability will be necessary. In addition, exhaust nozzle functions, in all probability, will be shared by both the engine and aircraft control systems. Advanced technology exhaust system development status, including full scale and model scale test results, will be discussed in this paper.
Authors
Citation
Dusa, D., Speir, D., and Dunbar, D., "Multi-Functional Nozzle For Advanced Weapon Systems," SAE Technical Paper 831426, 1983, https://doi.org/10.4271/831426.Also In
References
- Dusa, D.J. Speir, D.W. Rowe, R.K. Leavitt, L.D. “Advanced Technology Exhaust Nozzle Development” AIAA-83-1286 June 1983
- Hiley, P.E. Bowers, D.L. “Advanced Nozzle Integration for Supersonic Strike Fighter Application” AIAA-81-1441 July 1981
- Taylor, R.P. Lander, J.A. “Recent Advances in Thrust Vectoring Systems” AGARD Conference Preprint No. 135
- Nash, D.O. Wakeman, T.G. Palcza, J. L. “Structural and Cooling Aspects of the ADEN Nonaxisymmetric Exhaust Nozzle” ASHE Paper 77-GT-110 Jan. 7 1976
- Schnell, W.C. Grossman, R.L. Hoff, G.E. “Comparison of Non-Axisymmetric & Axisymmetric Nozzles Installed on a V/STOL Fighter Model” SAE Paper 770983 , November 1977
- Schnell, W.C. Grossman, R.L. “Vectoring Non-Axisymmetric Nozzle Jet Induced Effects on a V/STOL Fighter Model” AIAA Paper 78-1080 July 1978
- Straight, D.M. Cullom, R.R. “Performance of a 2DCD Nonaxisymmetric Exhaust Nozzle on a Turbojet Engine at Altitude” NASA TM 82881 June 1982