Side Force on Bodies of Revolution: Role of Attached Flow-Reference-Cited by-同舟云学术

Side Force on Bodies of Revolution: Role of Attached Flow

Published:2021-11 Issue:11 Volume:59 Page:4475-4485
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liaño Gabriel¹,Jiménez-Varona José¹

Affiliation:

1. National Institute of Aerospace Technology, 28850 Madrid, Spain

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060389

Reference32 articles.

1. LetkoW. “A Low Speed Experimental Study of the Directional Characteristics of a Sharp Nosed Fuselage Through a Large Angle of Attack Range at Zero Sideslip,” NACA TN 2911, 1953.

2. DunnE. L. “A Low Speed Experimental Study of Yaw Forces on Bodies of Revolution at Large Angles of Pitch and Zero Angle of Side Slip,” U.S. Naval Ordnance Test Station TM 1588, China Lake, CA, 1954.

3. PickG. S. “Investigation of Side Forces on Ogive-Cylinder Bodies at High Angles of Attack in the M=0.5 to 1.1 Range,” AIAA Paper 1971-0570, June 1971.

4. Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack

5. LamontP. J. “Pressure Measurements on an Ogive-Cylinder at High Angles of Attack with Laminar, Transitional, or Turbulent Separation,” AIAA Paper 1980-1556, Aug. 1980. 10.2514/6.1980-1556

Cited by 2 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. Fineness Ratio Effects on the Flow Past an Axisymmetric Body at High Incidence;Aerospace;2023-05-04

2. Roughness Effect on the Flow Past Axisymmetric Bodies at High Incidence;Aerospace;2022-10-28