Dynamic Stability Analysis of Blunt-Body Entry Vehicles Using Time-Lagged Aftbody Pitching Moments-Reference-Cited by-同舟云学术

Dynamic Stability Analysis of Blunt-Body Entry Vehicles Using Time-Lagged Aftbody Pitching Moments

Published:2015-03 Issue:2 Volume:52 Page:393-403
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Kazemba Cole D.¹,Braun Robert D.²,Schoenenberger Mark³,Clark Ian G.⁴

Affiliation:

1. Systems Analysis Branch, NASA Ames Research Center, Moffett Field, California 94035

2. Daniel Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0150

3. Exploration Systems Engineering Branch, NASA Langley Research Center, Hampton, Virginia 23681

4. Entry, Decent, and Landing Systems and Advanced Technologies Group, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

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.A32894

Reference19 articles.

1. ChapmanG. T.YatesL. A. “Dynamics of Planetary Probes: Design and Testing Issues,” AIAA Paper 1998-0797, Jan. 1998.

2. Survey of Blunt Body Dynamic Stability in Supersonic Flow

3. BeamB. H.HedstromE. C. “Damping in Pitch of Bluff Bodies of Revolution at Mach Numbers from 2.5 to 3.5,” NASA TM-X-90, Nov. 1959.

4. Numerical Analysis of Dynamic Stability of a Reentry Capsule at Transonic Speeds

5. Study for dynamically unstable motion of reentry capsule

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. Unsteady Aerodynamic Uncertainty Quantification of a Blunt-Body Entry Vehicle in Free-Flight;AIAA SCITECH 2024 Forum;2024-01-04

2. Aerodynamic Performance of the Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) Technology Demonstration Mission;AIAA SCITECH 2024 Forum;2024-01-04

3. Dynamic instability modeling on phase plane for thin aeroshell capsule with pitching motion at transonic speed;Mechanical Engineering Journal;2024

4. An augmented physics informed neural network approach for blunt-body dynamics;Physics of Fluids;2024-01-01

5. Dynamic Stability of Deployable Aeroshells at Supersonic Speeds;AIAA SCITECH 2023 Forum;2023-01-19