Get started
Author

Cindy W. Albertson

Observed names: Albertson, Cindy W., C. ALBERTSON, CINDY ALBERTSON, Cindy Albertson
OpenAlex ID: A5006758789
Mach 4 Test Results of a Dual-Flowpath, Turbine Based Combined Cycle Inlet
2006 · Cindy Albertson, Saied Emami, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 39
Shock Interaction Control for Scramjet Cowl Leading Edges
2005 · Cindy Albertson, Venki Venkat · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 17
Aircraft High-Lift Aerodynamic Analysis Using a Surface-Vorticity Solver
2016 · Erik D. Olson, Cindy W. Albertson · AIAA Aerospace Sciences Meeting · 15
Total temperature probes for high-temperature hypersonic boundary-layer measurements
1993 · Cindy W. Albertson, Willard A. Bauserman · NASA Technical Reports Server (NASA) · 13
PDF
Design of Two RadWorks Storm Shelters for Solar Particle Event Shielding
2014 · Matthew A. Simon, Jeffrey Cerro, et al. · AIAA SPACE Conference & Exposition · 11
PDF
End-To-End Simulation of Launch Vehicle Trajectories Including Stage Separation Dynamics
2012 · Cindy Albertson, Paul Tartabini, et al. · AIAA Atmospheric Flight Mechanics Conference · 10
PDF
Evaluation of Equilibrium Turbulence for a Hypersonic Boundary Layer at Nonadiabatic Wall Conditions
2024 · Albertson, Cindy W. · NASA STI Repository (National Aeronautics and Space Administration) · 7
PDF
Compressible Equilibrium Turbulent Boundary Layers at Nonadiabatic Wall Conditions
1991 · Cindy W. Albertson, Robert L. Ash · AIAA Journal · 3
Evaluation of equilibrium turbulence for a naturally developing hypersonic boundary layer at nonadiabatic wall conditions
1990 · CINDY ALBERTSON, ROBERT ASH · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 3
Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5.
1989 · Tony L. Parrott, M G Jones, et al. · 3
Development of Logistics for Building Radiation Storm Shelters and their Operational Evaluation
2015 · Jeffrey A. Cerro, Kara Latorella, et al. · AIAA SPACE Conference & Exposition · 2
PDF
Alleviation of facility/engine interactions in an open-jet scramjet test facility
2001 · Cindy Albertson, Saied Emami · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 2
Aerothermal environment of a blunted three-dimensional nonaxisymmetric body at Mach 6.8
1984 · F. MARTIN, JR., C. ALBERTSON · AIAA Thermophysics Conference · 2
Aerothermal evaluation of a spherically blunted body with a trapezoidal cross section in the Langley 8-foot high-temperature tunnel
1987 · Cindy W. Albertson · NASA Technical Reports Server (NASA) · 1
PDF
Aerothermal tests of a 12.5 percent cone at Mach 6.7 for various Reynolds numbers, angles of attack and nose shapes. [conducted in Langley 8-foot high temperature tunnel
1984 · Robert Nowak, Cindy W. Albertson, et al. · 1
Development of Constraint Force Equation Methodology for Application to Multi-Body Dynamics Including Launch Vehicle Stage Seperation
2016 · Bandu N. Pamadi, Matthew Toniolo, et al. · NASA STI Repository (National Aeronautics and Space Administration)
PDF
Aerothermal tests of a 12.5 percent cone at Mach 6.7 for various Reynolds numbers, angles of attack and nose shapes
1984 · Robert Nowak, Cindy W. Albertson, et al. · NASA STI Repository (National Aeronautics and Space Administration)
PDF
Blockage and flow studies of a generalized test apparatus including various wing configurations in the Langley 7-inch Mach 7 Pilot Tunnel
1982 · Cindy W. Albertson · NASA Technical Reports Server (NASA)
PDF
Works count: 22
Citation count: 129
H-index: 7
I10-index: 6
Year
Topic
Type