Mark E. Newfield

发表

Aerothermodynamic performance enhancement and design of sphere-cones using the artificially blunted leading edge concept

Anurag Gupta, Leslie Yates, Stephen M. Ruffin, 1999 .

THE REUSABLE LAUNCH VEHICLE CHALLENGE

Daniel J. Rasky, Mark E. Newfield, R. Bruce Pittman, 2006 .

Perspective on ReEntry Breakup Recorder Derived Concepts for Small Payload Flight Experiments

Daniel J. Rasky, Prabhakar Subrahmanyam, Mark E. Newfield, 2013 .

Reactivation and upgrade of the NASA Ames 16-Inch Shock Tunnel - Status report

David W. Bogdanoff, Robert J. Miller, Mark E. Newfield, 1992 .

Flow characterization in the NASA Ames 16-inch Shock Tunnel

David W. Bogdanoff, Mark E. Newfield, John A. Cavolowsky, 1992 .

ACCESS FROM SPACE: A NEW PERSPECTIVE ON NASA'S SPACE TRANSPORTATION NEEDS AND OPPORTUNITIES

Ethiraj Venkatapathy, Daniel J. Rasky, Mark E. Newfield, 2005 .

30 degree injectors at hypervelocity conditions

David W. Bogdanoff, Robert D. Bittner, Mark E. Newfield, 1992 .

Space Rush: The Case for Infrastructure-Based Space Exploration

Daniel J. Rasky, Mark E. Newfield, Lynn D. Harper, 2009 .

Spectroscopic Emission Measurements Within the Blunt-Body Shock Layer in an Arcjet Flow

Douglas G. Fletcher, Mark E. Newfield, Tahir Gokcen, 1998 .

Laser absorption flow diagnostics for use in hypersonic ground-based and flight experiments

Mark E. Newfield, John A. Cavolowsky, M. Newfield, 1992 .

Computational Analysis of Shock Layer Emission Measurements in an Arc-jet Facility

Douglas G. Fletcher, Mark E. Newfield, Tahir Gokcen, 1998 .