Hypersonic Boundary-Layer Trip Development for Hyper-X

By S. Berry, A. Auslender, A. Dilley, J. Calleja. 2000

206 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/b402e913c65ff4b2bee99a4b46630a89e6849f2b

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. S. Schneider
2. J. Bertin
3. R. Cummings

In Applied Mathematics

1. S. Schneider
2. R. Cummings
3. J. Bertin

In Computational Mechanics

1. S. Schneider
2. J. Bertin
3. R. Cummings

Citations in the corpus

• Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies (2004, background): “Scott Berry from NASA Langley has published aerothermodynamic measurements on the Hyper-X forebody [224, 223].”
• Effects of Roughness on Hypersonic Boundary-Layer Transition (2007, unknown): “[61] studied various types of trips, ending up with a particular swept-ramp vortex generator.”
• Critical Hypersonic Aerothermodynamic Phenomena (2006, background): “And one article by Berry et al. (2001b) related to objective 5: “Obtain data that can be used to develop empirical correlations for phenomena that resist analytical and/or numerical modeling, such as boundary-layer transition and turbulence modeling.””