Matching inviscid/boundary-layer flowfields-Reference-Cited by-同舟云学术

Matching inviscid/boundary-layer flowfields

Published:1996-01 Issue:1 Volume:34 Page:35-42
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

DeJarnette Fred R.¹,Radcliffe Robert A.¹

Affiliation:

1. North Carolina State University, Raleigh, North Carolina 27695-7910

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.13018

Reference11 articles.

1. Application of axisymmetric analog for calculating heating in three-dimensional flows

2. Approximate Convective-Heating Equations for Hypersonic Flows

3. Engineering calculations of three-dimensional inviscid hypersonic flowfields

4. An engineering aerodynamic heating method for hypersonic flow

5. 5Riley, C. J. "An Engineering Method for Interactive Inviscid-Boundary Layers in Three-Dimensional Hypersonic Flows," Ph.D. Dissertation, Dept. of Mechanical and Aerospace Engineering,North Carolina State Univ., Raleigh, NC,May 1992.

Cited by 4 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. Approximations of the Navier–Stokes equations for high Reynolds number flows past a solid wall;Journal of Computational and Applied Mathematics;2004-04

2. Memoirs: Obtaining the Right Solution to Thermophysics Problems;Journal of Spacecraft and Rockets;2003-07

3. On Kaplun limits and the generalized boundary layer theory;International Journal of Engineering Science;2002-09

4. Obtaining the Right Solution to Thermophysics Problems;32nd AIAA Fluid Dynamics Conference and Exhibit;2002-06-24