A Method for Reducing Sonic Boom Strength by Tailoring the Shape of the Propulsive Streamtube-Reference-Cited by-同舟云学术

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A Method for Reducing Sonic Boom Strength by Tailoring the Shape of the Propulsive Streamtube

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
Short-container-title:

Author:

Conners Timothy R.¹,Henne Preston¹,Howe Donald C.¹

Affiliation:

1. Gulfstream Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3678

Reference36 articles.

1. 1Mack,R.J."ASupersonicBusiness-JetConceptDesignedforLowSonicBoom,"NASATM-2003-212435,Oct.2003.

2. 3Conners,T.R.,Howe,D.C.,andWhurr,J.R."ImpactofEngineCycleSelectiononPropulsionSystemIntegrationand VehiclePerformance for aQuiet SupersonicAircraft,"AIAAPaper 2005-1016, 2005.

3. 4Conners,T.R.,Howe,D.C.,Whurr,J.R.,andSmith,C.F."ConceptualDesign,Integration,andDevelopmentPlanforan Efficient LowSonicBoomPropulsionSystemEmploying Advanced SupersonicEngineCycles,"Final Report-Public Distribution, NASAContract NNC04CA29C, amended Aug. 27,2007.

Cited by 3 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. Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion;AIAA Aviation 2019 Forum;2019-06-14

2. Viscous Aerodynamic Shape Optimization with Installed Propulsion Effects;35th AIAA Applied Aerodynamics Conference;2017-06-02

3. Aerodynamic Shape Optimization of a Two-Stream Supersonic Plug Nozzle;53rd AIAA Aerospace Sciences Meeting;2015-01-03

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