Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment

By B. Reinartz, C. Herrmann, J. Ballmann, W. Koschel. 2003

205 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/98789033b64ac93b1bdf53191485530fe74514ad

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. N. Clemens
2. D. Dolling
3. Venkat Narayanaswamy
4. E. Touber
5. Neil D. Sandham
6. B. W. van Oudheusden
7. Fulvio Scarano
8. Bharathram Ganapathisubramani

In Applied Mathematics

1. N. Clemens

In Computational Mechanics

1. N. Clemens
2. D. Dolling
3. Bharathram Ganapathisubramani
4. Venkat Narayanaswamy
5. Fulvio Scarano
6. B. W. van Oudheusden
7. Neil D. Sandham
8. E. Touber

Citations in the corpus

• Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow (2009, methodology): “length [4,7–11], isolator aspect ratio [13], isolator entrance flow”
• Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves (2012, methodology): “b Double contour-induced shocks by the cowl (Reinartz et al. 2003) 1648 Exp Fluids (2012) 53:1647–1661”