K. Suder

发表

Experimental Study of Bypass Transition in a Boundary Layer. M.S. Thesis

Kenneth L. Suder, Eli Reshotko, E. Reshotko, 1988 .

Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part II — Circumferential Distortion

James D. Paduano, Zoltán S. Spakovszky, H. J. Weigl, 1998 .

NASA's Role in Gas Turbine Technology Development: Accelerating Technical Progress Via Collaboration Between Academia, Industry, and Government Agencies

K. Suder, 2019, Journal of Turbomachinery.

Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss

K. Suder, 2013 .

Vision 2030 Aircraft Propulsion Grand Challenge Problem: Full-engine CFD Simulations with High Geometric Fidelity and Physics Accuracy

G. Laskowski, G. Medic, Umesh Paliath, 2020, AIAA Scitech 2021 Forum.

Laser anemometer measurements in a transonic axial-flow fan rotor

Michael D. Hathaway, J. R. Wood, Anthony J. Strazisar, 1989 .

Results of an Advanced Fan Stage Operating Over a Wide Range of Speed and Bypass Ratio. Part 2; Comparison of CFD and Experimental Results

Sameer Kulkarni, Mark L. Celestina, Kenneth L. Suder, 2010 .

The effect of adding roughness and thickness to a transonic axial compressor rotor

W. B. Roberts, Anthony J. Strazisar, William B. Roberts, 1994 .

Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor

Mark L. Celestina, Kenneth L. Suder, M. Celestina, 1994 .

Compressor Stability Enhancement Using Discrete Tip Injection

Michael D. Hathaway, Scott A. Thorp, Anthony J. Strazisar, 2000 .

An Overview of the NASA FAP Hypersonics Project Airbreathing Propulsion Research

Scott R. Thomas, Kenneth L. Suder, A. H. Auslender, 2009 .

Near-Field Acoustic Power Level Analysis of F31/A31 Open Rotor Model at Simulated Cruise Conditions

K. Suder, 2015 .

Overview of the NASA Environmentally Responsible Aviation Project's Propulsion Technology Portfolio

Kenneth L. Suder, K. Suder, 2012 .