Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow-Reference-Cited by-同舟云学术

Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow

Published:1980-11 Issue:6 Volume:17 Page:529-536
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

DeJarnette F. R.¹,Ford C. P.¹,Young D. E.²

Affiliation:

1. North Carolina State University, Raleigh, N. C.

2. Naval Surface Weapons Center, Dahlgren, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.57770

Reference11 articles.

1. 3Syvertson, C.A. and Dennis, D.H. "A Second-Order Shock-Expansion Method Applicable to Bodies of Revolution Near Zero Lift," NACA Report 1328, 1957.

2. Development of a Computer Program to Calculate Aerodynamic Characteristics of Bodies and Wing-Body Combinations.

Cited by 12 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. Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression;Aerospace Science and Technology;2024-01

2. Exact relation for determining the pressure distribution on a sphere at an arbitrary mach number in a supersonic incoming flow;Mathematical Models and Computer Simulations;2015-03

3. Missile DATCOM Transonic Drag Improvements for Hemispherical Nose Shapes;21st AIAA Applied Aerodynamics Conference;2003-06-21

4. Applications of a Counterflow Drag Reduction Technique in High-Speed Systems;Journal of Spacecraft and Rockets;2002-07

5. Applications of a counterflow drag reduction technique in high speed systems;19th AIAA Applied Aerodynamics Conference;2001-06-11