Design of Modular Shape-Transition Inlets for a Conical Hypersonic Vehicle-Reference-Cited by-同舟云学术

Design of Modular Shape-Transition Inlets for a Conical Hypersonic Vehicle

Published:2013-07 Issue:4 Volume:29 Page:832-838
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Gollan Rowan J.¹,Smart Michael K.¹

Affiliation:

1. School of Mechanical and Mining Engineering, University of Queensland, Brisbane, Queensland 4072, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34672

Reference13 articles.

1. PinckneyS. Z. “Rectangular Capture Area to Circular Combustor,” NASA Langley Research Center TM-78657, Hampton, VA, 1978.

2. Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition

3. HartillW. B. “Analytical and Experimental Investigation of a Scramjet Inlet of Quadriform Shape,” Marquardt Corp., U.S. Air Force, Van Nuys, California, TR-AFAPL-TR-65-74, Aug. 1965.

4. KierseyJ. L.SnowM. L. “Modular Inlet Investigation,” Aeronautics Div., Research and Development, Applied Physics Lab., Johns Hopkins Univ., Quarterly Rept. AQR/66-1, Baltimore, MD, Jan. 1966.

5. MölderS.RomeskieJ. M. “Modular Hypersonic Inlets with Conical Flow,” McGill Univ., AGARD CP-30, Montreal, 1968.

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