High-Alpha Prediction of Roll Damping and Magnus Stability Coefficients for Finned Projectiles-Reference-Cited by-同舟云学术

High-Alpha Prediction of Roll Damping and Magnus Stability Coefficients for Finned Projectiles

Published:2016-07 Issue:4 Volume:53 Page:720-729
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Bhagwandin Vishal A.¹

Affiliation:

1. U.S. Army Research Laboratory, Aberdeen Proving Ground, Maryland 21005

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33419

Reference29 articles.

1. JenkeL. M. “Experimental Roll-Damping, Magnus, and Static-Stability Characteristics of Two Slender Missile Configurations at High Angles of Attack (0–90 deg) and Mach Numbers 0.2 Through 2.5,” Arnold Engineering and Development Center Rept. AEDC-TR-76-58, Arnold Air Force Base, Tennessee, July 1976.

2. DupuisA. D.HathawayW. “Aeroballistic Range Tests of the Basic Finner Reference Projectile at Supersonic Velocities,” Defense Research Establishment Rept. DREV-TM-9703, Valcartier, QBC, Canada, Aug. 1997.

3. DupuisA. “Aeroballistic Range and Wind Tunnel Tests of the Basic Finner Reference Projectile from Subsonic to High Supersonic Velocities,” Defense R&D Canada TM 2002-136, Valcartier, QBC, Canada, Oct. 2002.

4. DupuisA. D.HathawayW. “Aeroballistic Range Tests of the Air Force Finner Reference Projectile,” Defense R&D Canada TM 2002-008, Valcartier, QBC, Canada, May 2002.

5. WestK. O. “Comparison of Free Flight Spark Range and Wind Tunnel Test Data for a Generic Missile Configuration at Mach Numbers from 0.6 to 2.5,” U.S. Air Force Armament Lab. Rept. AFATL-TR-81-87, Eglin AFB, FL, Oct. 1981.

Cited by 16 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. Numerical Investigation of Basic Finner Model in Roll Motion as Complement to the Experimental Work;AIAA SCITECH 2024 Forum;2024-01-04

2. Coherent solutions to roll damping derivatives evaluation for a generic rocket model;INCAS BULLETIN;2023-09-04

3. Research on rolling stability of the flexible waverider based on computational fluid dynamics/computational structural dynamics/rigid body dynamics coupling methodology;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-12-27

4. Parametric Study on Lateral–Directional Stability of Hypersonic Waverider;AIAA Journal;2021-06-14

5. Comparison of Aeroprediction Methods for Guided Munitions;AIAA Scitech 2021 Forum;2021-01-04