Mechanism of Side Force Generation and Its Alleviation over a Slender Body-Reference-Cited by-同舟云学术

Mechanism of Side Force Generation and Its Alleviation over a Slender Body

Published:2016-01 Issue:1 Volume:53 Page:195-208
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Kumar P.¹,Prasad J. K.¹

Affiliation:

1. Birla Institute of Technology, Mesra, Ranchi 835 215, Jharkhand, India

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.A33290

Reference38 articles.

1. Prediction of aerodynamic out-of-plane forces on ogive-nosed circular cylinders

2. KeenerE. R.ChapmanG. T.CohenL.TaleghaniJ. “Side Force on a Tangent Ogive Forebody with Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7,” NASA TM-X-3437, Feb. 1977.

3. Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation

4. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream

5. The effect of roll angle on the flow over a slender body of revolution at high angles of attack

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