Pressure Fluctuations (Buzzing) and Inlet Performance of an Airbreathing Missile-Reference-Cited by-同舟云学术

Pressure Fluctuations (Buzzing) and Inlet Performance of an Airbreathing Missile

Published:2013-07 Issue:4 Volume:29 Page:839-848
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Herrmann Dirk¹,Siebe Frank¹,Gülhan Ali¹

Affiliation:

1. Supersonic and Hypersonic Technologies Department of the Institute of Aerodynamic and Flow Technology, DLR, German Aerospace Center, 51147 Cologne, Germany

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.B34629

Reference43 articles.

1. AIAA Education Series;Seddon J.,1985

2. AIAA Education Series;Seddon J.,1993

3. FisherS. A.NealeM. C.BrooksA. J. “On the Sub-Critical Stability of Variable Ramp Intakes at Mach Numbers Around 2,” National Gas Turbine Establishment, Rept. No. ARC/R&M-3711, Feb. 1970.

4. OswatitschK. “Der Druckrückgewinn bei Geschossen mit Rückstoßantrieb bei hohen Überschallgeschwindigkeiten (Der Wirkungsgrad von Stoßdiffusoren),” Forschungen und Entwicklungen des Heereswaffenamtes, Rept. 1005, Göttingen, Germany, 1944;

5. Hypersonic Airbreathing Propulsion

Cited by 35 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic Instabilities in High-Speed Air Intakes and Their Role in Propulsion System Integration;Aerospace;2024-01-12

2. Analysis of unsteady pressure measurements in the unstart of a Mach 6.58 hypersonic intake;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

3. Computation of viscous flow characteristics of a supersonic intake using eddy-viscosity turbulence models;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-07-06

4. Investigation of Shock Wave Oscillation Suppression by Overflow in the Supersonic Inlet;Energies;2022-05-24

5. Supersonic inlet flow recognition by hybrid-mutation non-dominated sorting genetic algorithm with support vector machines;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-05-15