Base drag prediction on missile configurations-Reference-Cited by-同舟云学术

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Base drag prediction on missile configurations

Published:1993-08-09 Issue: Volume: Page:
ISSN:
Container-title:Flight Simulation and Technologies
language:
Short-container-title:

Author:

MOORE F.¹,HYMER T.¹,WILCOX F.²

Affiliation:

1. U.S. Navy, Naval Surface Warfare Center, Dahlgren, VA

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3629

Reference28 articles.

1. Devan,L.;andMason,L.,Aerodynamicsof mtical WeaponstoMachNumber 8andAngle ofAttack 180":Part 11,ComputerProgram and UsersGuide,NSWCTR81-358,September 1981.

2. Love,E.S.,BasePressureatSupersonicSpeeds on Two-DimensionalAirfoils andonBodies of Revolution with andwithout TurbulentBoundaryLayers,NACA TN3819.1957.

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1. CFD Study of Base Drag of the Grot Rocket;Transactions on Aerospace Research;2023-06-01

2. Influence of swirl on the supersonic wake flow structure behind blunt-based axisymmetric afterbodies;Journal of Fluid Mechanics;2021-08-27

3. The Direct Measurement of Base Drag for Hypersonic Vehicles;29th International Symposium on Shock Waves 1;2015

4. Velocity measurements in a three-dimensional compressible base flow;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

5. An improved semiempirical method for power-on base drag prediction;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2001-08-06

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