Relevant bibliographies by topics / Air-breathing propulsion

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Air-breathing propulsion'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 February 2022

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Air-breathing propulsion.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Air-breathing propulsion"

1

PATNAIK, SURYA N., THOMAS M. LAVELLE, and DALE A. HOPKINS. "Optimization of air-breathing propulsion engine concept." Communications in Numerical Methods in Engineering 13, no. 8 (August 1997): 635–41. http://dx.doi.org/10.1002/(sici)1099-0887(199708)13:8<635::aid-cnm89>3.0.co;2-x.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Shi Lei, 石磊, 赵尚弘 Zhao Shanghonh, 周万银 Zhou Wanyin, 李勇军 Li Yongjun, 胥杰 Xu Jie, and 方绍强 Fang Shaoqiang. "Numerical Analysis of Air-Breathing Mode Laser Propulsion." Chinese Journal of Lasers 35, no. 1 (2008): 49–54. http://dx.doi.org/10.3788/cjl20083501.0049.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Schoettle, U. M., H. Grallert, and F. A. Hewitt. "Advanced air-breathing propulsion concepts for winged launch vehicles." Acta Astronautica 20 (January 1989): 117–29. http://dx.doi.org/10.1016/0094-5765(89)90061-1.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Marchioni, Francesco, and Mark A. Cappelli. "Extended channel Hall thruster for air-breathing electric propulsion." Journal of Applied Physics 130, no. 5 (August 7, 2021): 053306. http://dx.doi.org/10.1063/5.0048283.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Zhang, Xi-bin, and Qun Zong. "Modeling and Analysis of an Air-Breathing Flexible Hypersonic Vehicle." Mathematical Problems in Engineering 2014 (2014): 1–9. http://dx.doi.org/10.1155/2014/264247.

Full text
Abstract:
By using light-weighted material in hypersonic vehicle, the vehicle body can be easily deformed. The mutual couplings in aerodynamics, flexible structure, and propulsion system will bring great challenges for vehicle modeling. In this work, engineering estimated method is used to calculate the aerodynamic forces, moments, and flexible modes to get the physics-based model of an air-breathing flexible hypersonic vehicle. The model, which contains flexible effects and viscous effects, can capture the physical characteristics of high-speed flight. To overcome the analytical intractability of the model, a simplified control-oriented model of the hypersonic vehicle is presented with curve fitting approximations. The control-oriented model can not only reduce the complexity of the model, but also retain aero-flexible structure-propulsion interactions of the physics-based model and can be applied for nonlinear control.
APA, Harvard, Vancouver, ISO, and other styles
6

Göksel, B., and I. Ch Mashek. "First Breakthrough for Future Air-Breathing Magneto-Plasma Propulsion Systems." Journal of Physics: Conference Series 825 (April 12, 2017): 012005. http://dx.doi.org/10.1088/1742-6596/825/1/012005.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Sundaresan, M. "Design aspects of launch vehicle sizing including air-breathing propulsion." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 220, no. 5 (May 2006): 487–98. http://dx.doi.org/10.1243/09544100jaero30.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Bussard, Robert W., and Lorin W. Jameson. "Inertial-Electrostatic-Fusion Propulsion Spectrum: Air-Breathing to Interstellar Flight." Journal of Propulsion and Power 11, no. 2 (March 1995): 365–72. http://dx.doi.org/10.2514/3.51434.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Urzay, Javier. "Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight." Annual Review of Fluid Mechanics 50, no. 1 (January 5, 2018): 593–627. http://dx.doi.org/10.1146/annurev-fluid-122316-045217.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Mukundan, Vijith, Arnab Maity, Shashi Ranjan Kumar, and U. P. Rajeev. "Ascent Trajectory Optimization of Launch Vehicles with Air-Breathing Propulsion." IFAC-PapersOnLine 52, no. 12 (2019): 274–79. http://dx.doi.org/10.1016/j.ifacol.2019.11.255.

Full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Air-breathing propulsion"

1

Wilhite, Jarred M. "Investigation of Various Novel Air-Breathing Propulsion Systems." University of Cincinnati / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ucin147981623341895.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Singh, Lake Austin. "Very low earth orbit propellant collection feasibility assessment." Diss., Georgia Institute of Technology, 2014. http://hdl.handle.net/1853/53039.

Full text
Abstract:
This work focuses on the concept of sustainable propellant collection. The concept consists of gathering ambient gas while on-orbit and using it as propellant. Propellant collection could potentially enable operation in very-low Earth orbits without compromising spacecraft lifetime. This work conducts a detailed analysis of propellant collection from a physics perspective in order to test the assertions of previous researchers that propellant collection can dramatically reduce the cost of propellant on-orbit. Major design factors for propellant collection are identified from the fundamental propellant collection equations, which are derived in this work from first principles. A sensitivity analysis on the parameters in these equations determines the relative importance of each parameter to the overall performance of a propellant-collecting vehicle. The propellant collection equations enable the study of where propellant collection is technically feasible as a function of orbit and vehicle performance parameters. Two case studies conducted for a very-low Earth orbit science mission and a propellant depot-type mission serve to demonstrate the application of the propellant collection equations derived in this work. The results of this work show where propellant collection is technically feasible for a wide range of orbit and vehicle performance parameters. Propellant collection can support very-low Earth operation with presently available technology, and a number of research developments can further extend propellant-collecting concepts' ability to operate at low altitudes. However, propellant collection is not presently suitable for propellant depot applications due to limitations in power.
APA, Harvard, Vancouver, ISO, and other styles
3

Olsen, Jon. "Spillage Drag Estimation and Drag-Thrust Accounting for a Missile with Air Breathing Propulsion." Thesis, KTH, Flygdynamik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-102075.

Full text
Abstract:
Air intake related aerodynamic aspects of an air breathing cruise missile are analyzed. A method for thrust and drag accounting is established, and, based on that, a partial simulation model for the thrust and intake spillage drag force of the missile is developed. The model combines wind tunnel data with analytical data. The intake spillage force has two components, pre entry force and cowl force. The pre entry force can be computed relatively easily, while the cowl force depends strongly upon actual intake geometry and no general method exists. An approximate cowl force is computed based on available data. The accuracy of the cowl drag results is difficult to predict, as no complete theoretical model is available, and the partial models published cite no accuracy limits. The cowl drag results need further verification through wind tunnel tests or CFD analysis. However, spillage force results are produced that are in the magnitude of 30% of total drag, which is expected. Also, dependencies on known variables and trends are as expected. Finally, flight test profiles in order to validate the model are suggested.
APA, Harvard, Vancouver, ISO, and other styles
4

Wilson, Althea Grace. "Numerical study of energy utilization in nozzle/plume flow-fields of high-speed air-breathing vehicles." Diss., Rolla, Mo. : Missouri University of Science and Technology, 2008. http://scholarsmine.mst.edu/thesis/pdf/Wilson_09007dcc804d881b.pdf.

Full text
Abstract:
Thesis (M.S.)--Missouri University of Science and Technology, 2008.
Vita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed April 25, 2008) Includes bibliographical references (p. 57).
APA, Harvard, Vancouver, ISO, and other styles
5

Lewis, Mark Joel. "The prediction of inlet flow stratification and its influence on the performance of air-breathing hypersonic propulsion systems." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/14370.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Song, Yangkun. "Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion." Diss., Virginia Tech, 2016. http://hdl.handle.net/10919/93960.

Full text
Abstract:
Foreign object ingestion (FOI) into jet engines is a recurring scenario during the operation life of aircraft. Objects can range from as small as a pebble on the tarmac to the size of a large bird. Among the potential ingestion scenarios, damage caused by smaller objects may be considered to be negligible. Alternatively, larger objects can initiate progressive damage, potentially leading to catastrophic failure, compromising the integrity of the structure, and endangering the safety of passengers. Considering the dramatic increase in air traffic, FOI represents a crucial safety hazard, and must be better understood to minimize possible damage and structural failure. The main purpose of this study is to develop a unique methodology to assess the response and dynamic damage progression of an advanced, high-bypass propulsion system in the event of an FOI during operation. Using a finite element framework, a unique modeling methodology has been proposed in order to characterize the FOI response of the system. In order to demonstrate versatility of the computational analysis, the impact characteristics of two most common foreign object materials, bird and ice, were investigated. These materials were then defined in finite element domain, verified computationally, and then validated against the existing physical experiments. In addition to the mechanics of the two FOI materials, other material definitions, used to characterize the structures of the high-bypass propulsion system, were also explored. Both composite materials and rate dependent definitions for metal alloys were investigated to represent the damage mechanics in the event of an FOI. Subsequently, damage sequence of high-bypass propulsion systems subject to FOI was developed and assessed, using a uniquely devised Fluid-Structure Interaction (FSI) technique. Using advanced finite element formulation, this approach enabled the accurate simulation of the comprehensive damage progression of the propulsion systems by including aerodynamic interaction. Through this strategy, fluid mechanics was combined with structural mechanics in order to simulate the mutual interaction between both continua, allowing the interpretation of both the additional damage caused by the fluid flow and disrupted aerodynamics induced by the dynamic deformation of the fan blade. Subsequently, this multidisciplinary-multiphysics computational approach, in the framework of the comprehensive analysis methodology introduced, enabled the effective determination of details on the overall progressive impact damage, not traditionally available to propulsion designers.
PHD
APA, Harvard, Vancouver, ISO, and other styles
7

Benyo, Theresa L. "Analytical and Computational Investigations of a Magnetohydrodynamic (MHD) Energy-Bypass System for Supersonic Turbojet Engines to Enable Hypersonic Flight." Kent State University / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=kent1369153719.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Williams, Nehemiah Joel. "A Performance Analysis of a Rocket Based Combined Cycle (RBCC) Propulsion System for Single-Stage-To-Orbit Vehicle Applications." 2010. http://trace.tennessee.edu/utk_gradthes/842.

Full text
Abstract:
Rocket-Based Combined Cycle (RBCC) engines combine the best performance characteristics of air-breathing systems such as ramjets and scramjets with rockets with the goal of increasing payload/structure and propellant performance and thus making LEO more readily accessible. The idea of using RBCC engines for Single-Stage-To-Orbit (SSTO) trans-atmospheric acceleration is not new, but has been known for decades. Unfortunately, the availability of detailed models of RBCC engines is scarce. This thesis addresses the issue through the construction of an analytical performance model of an ejector rocket in a dual combustion propulsion system (ERIDANUS) RBCC engine. This performance model along with an atmospheric model, created using MATLAB was designed to be a preliminary `proof-of-concept' which provides details on the performance and behavior of an RBCC engine in the context of use during trans-atmospheric acceleration, and also to investigate the possibility of improving propellant performance above that of conventional rocket powered systems. ERIDANUS behaves as a thrust augmented rocket in low speed flight, as a ramjet in supersonic flight, a scramjet in hypersonic flight, and as a pure rocket near orbital speeds and altitudes. A simulation of the ERIDANUS RBCC engine's flight through the atmosphere in the presence of changing atmospheric conditions was performed. The performance code solves one-dimensional compressible flow equations while using the stream thrust control volume method at each station component (e.g. diffuser, burner, and nozzle) in all modes of operation to analyze the performance of the ERIDANUS RBCC engine. Plots of the performance metrics of interest including specific impulse, specific thrust, thrust specific fuel consumption, and overall efficiency were produced. These plots are used as a gage to measure the behavior of the ERIDANUS propulsion system as it accelerates towards LEO. A mission averaged specific impulse of 1080 seconds was calculated from the ERIDANUS code, reducing the required propellant mass to 65% of the gross lift off weight (GLOW), thus increasing the mass available for the payload and structure to 35% of the GLOW. Validation of the ERIDANUS RBCC concept was performed by comparing it with other known RBCC propulsion models. Good correlation exists between the ERIDANUS model and the other models. This indicates that the ERIDANUS RBCC is a viable candidate propulsion system for a one-stage trans-atmospheric accelerator.
APA, Harvard, Vancouver, ISO, and other styles

Books on the topic "Air-breathing propulsion"

1

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Airbreathing propulsion for missiles and projectiles. Neuilly sur Seine, France: AGARD, 1992.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
2

Mehta, Unmeel B. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
3

O'Brien, C. J. Advanced earth-to-orbit propulsion concepts. New York: AIAA, 1986.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
4

Penaranda, Frank E. Aeronautical facilities catalogue. vol.2 Airbreathing propulsion and flight simulators. Washington: U.S. Office of Aeronautics and Space Technology, 1985.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
5

International Symposium on Air Breathing Engines (12th 1995 Melbourne, Vic.). Twelfth International Symposium on Air Breathing Engines: Symposium papers, September 10-15, 1995, Melbourne, Australia. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
6

National Conference on Air Breathing Engines and Aerospace Propulsion (7th 2004 I.I.T., Kanpur). Air breathing engines and aerospace propulsion: Proceedings of NCABE 2004, 05-07 November, 2004. Edited by Raghunandan B. N, Oommen Charlie, Sullerey R. K, and Indian Institute of Technology (Kānpur, India). New Delhi: Allied Publishers, 2004.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
7

International, Symposium on Air Breathing Engines (10th 1991 Nottingham England). Tenth International Symposium on Air Breathing Engines: Symposium papers, September 1-6, 1991, Nottingham, England. Wash., D.C: American Institute of Aeronautics and Astronautics, 1991.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
8

International Symposium on Air Breathing Engines (7th 1985 Peking, China). Seventh International Symposium on Air Breathing Engines: Symposium papers, September 2-6, 1985, Beijing, People's Republic of China. New York: American Institute of Aeronautics, 1985.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
9

Roche, Joseph M. Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
10

NASA Glenn Research Center's hypersonic propulsion program. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Air-breathing propulsion"

1

Rezunkov, Yuri A. "Basic Gas-Dynamic Theories of the Laser Air-Breathing and Rocket Propulsion." In High Power Laser Propulsion, 43–91. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-79693-8_2.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Bushnell, Dennis M. "Mixing and Combustion Issues in Hypersonic Air-Breathing Propulsion." In ICASE/LaRC Interdisciplinary Series in Science and Engineering, 3–16. Dordrecht: Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-011-1050-1_1.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Peng, Yuchuan, Huiqi Zheng, Hao Li, Zhong Peng, Hua Zhao, Qiongying Ren, Tao Li, and Liang Ding. "Design of Air-Breathing Electrical Propulsion Based on Cargo-Spacecraft for Replenishment." In Lecture Notes in Electrical Engineering, 441–49. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-33-4102-9_54.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Che Idris, Azam, Mohd Rashdan Saad, and Konstantinos Kontis. "Investigation of Variable Geometry Intake to Mitigate Unwanted Shock-Shock Interactions in a Hypersonic Air-Breathing Propulsion Device." In Lecture Notes in Mechanical Engineering, 71–79. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-4756-0_7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

"Air- Breathing Propulsion." In Aerospace Engineering Pocket Reference, 299–308. CRC Press, 2015. http://dx.doi.org/10.1201/b18185-26.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

"Hypersonic Air-Breathing Propulsion." In Eleven Seconds into the Unknown, 51–74. Reston ,VA: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/5.9781600867774.0051.0074.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

"Air-Breathing Propulsion Flowpath Applications." In Fundamentals and Applications of Modern Flow Control, 373–402. Reston ,VA: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/5.9781563479892.0373.0402.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Sforza, Pasquale M. "Combustion Chambers for Air-Breathing Engines." In Theory of Aerospace Propulsion, 127–59. Elsevier, 2012. http://dx.doi.org/10.1016/b978-1-85617-912-6.00004-9.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Yang, V., F. H. Ma, and J. Y. Choi. "SYSTEM PERFORMANCE AND THRUST CHAMBER OPTIMIZATION OF AIR-BREATHING PULSE DETONATION ENGINES." In Combustion Processes in Propulsion, 397–406. Elsevier, 2006. http://dx.doi.org/10.1016/b978-012369394-5/50041-x.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

"Propulsion System Performance and Integration for High Mach Air Breathing Flight." In High-Speed Flight Propulsion Systems, 101–42. Washington DC: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/5.9781600866104.0101.0142.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Air-breathing propulsion"

1

MATTINGLY, JACK. "Air breathing propulsion education software for PCs." In 24th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2977.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

JOSHI, PRAKASH, EDMOND LO, and EVAN PUGH. "Laser-driven hypersonic air-breathing propulsion simulator." In 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3922.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

"Thermal management of air-breathing propulsion systems." In 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-514.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

TOWNEND, L. "Base pressure control for air-breathing launchers." In 26th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-1936.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Kim, Young-Taek. "Micro Supersonic Air-Breathing Laser- Spike Engine Propulsion." In BEAMED ENERGY PROPULSION: Fourth International Symposium on Beamed Energy Propulsion. AIP, 2006. http://dx.doi.org/10.1063/1.2203251.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

PHILLIPS, STEPHEN, and DUANE MATTERN. "Feedback linearization for control of air breathing engines." In 27th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2000.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

DORRINGTON, G. "Optimum directions for air-breathing launch vehicle design." In 23rd Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1818.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

"Restart of theory of air-breathing engines." In 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3472.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Kentfield, J. "Thermodynamics of air-breathing pulse-detonation engines." In 37th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3982.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Lytle, John. "Multi-fidelity Simulations of Air Breathing Propulsion Systems." In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-4967.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Reports on the topic "Air-breathing propulsion"

1

Tan, Choon S., Kenneth Breuer, Thomas Corke, Jin-Woo Bae, and Robert Bayt. MEMS-Based Control for Air-Breathing Propulsion. Fort Belvoir, VA: Defense Technical Information Center, March 2001. http://dx.doi.org/10.21236/ada387696.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

White, James H., James A. Marvin, and Anthony F. Sammells. Novel Electrolytes for the Electrochemical Machining of Air-Breathing Propulsion Materials. Fort Belvoir, VA: Defense Technical Information Center, January 1996. http://dx.doi.org/10.21236/ada370624.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

OFFICE OF NAVAL RESEARCH ARLINGTON VA. Naval Research Reviews. Mixing Enchancement for Air-Breathing Propulsion. Non-Axisymmetric Jets Increase Mixing. Volume 44 and Volume 45. Fort Belvoir, VA: Defense Technical Information Center, January 1993. http://dx.doi.org/10.21236/ada268966.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Air-breathing propulsion' for particular source types:
Journal articles Books
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography