Double-Jet Ejection of Cooling Air for Improved Film Cooling

By K. Kusterer, D. Bohn, T. Sugimoto, Ryozo Tanaka. 2007

169 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/f04838731e5467dc9be8fa4ec163c60e8b4df782

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. Je-Chin Han
2. Akhilesh P. Rallabandi

In Computational Mechanics

1. Je-Chin Han
2. Akhilesh P. Rallabandi

In Mechanical Engineering

1. Je-Chin Han
2. Akhilesh P. Rallabandi

Citations in the corpus

• ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE (2014, unknown): “Geometries included conical, laidback, and fanshaped holes [2-6], and many novel designs: bean-shaped [7], cusp-shaped [8], crescent-shaped [9], cratered [10], “Console” [11], double-jet [12], Nekomimi [13], transonic wall jet [14], waist-shaped [15], arrowhead-shaped [16], and anti-vortex holes [17”
• TURBINE BLADE FILM COOLING USING PSP TECHNIQUE (2010, background): “More recently, Kusterer et al. (2007) studied two rows of film cooling holes with opposite orientation and internal supply geometries.”