LTN Inlets and Nozzles Branch Overview; NASA GE - Methods Development Review
Lessons Learned from Inlet Integration Analysis of NASA's Low Boom Flight Demonstrator
Effects of Spent Cooling and Swirler Angle on a 9-Point Swirl-Venturi Injector
Lessons Learned During TBCC Design for the NASA-AFRL Joint System Study
Aerodynamic Investigation of Incidence Angle Effects in a Large Scale Transonic Turbine Cascade
Computational Analysis of a Low-Boom Supersonic Inlet
Results of an Advanced Fan Stage Operating Over a Wide Range of Speed and Bypass Ratio, Part 2
Design and Calibration of a Flowfield Survey Rake for inlet Flight Research
AMBR (Advanced Material Bipropellant Rocket) Engine for Science Missions
100-Lb(f) LO2/LCH4 Reaction Control Engine Technology Development for Future Space Vehicles
Beach Erosion Mitigation and Sediment Management Alternatives at Wallops Island, VA
Parametric Inlet Tested in Glenn's 10- by 10-Foot Supersonic Wind Tunnel
Aerial Surveys of Belugas in Cook Inlet, Alaska, June 2001, 2002, 2003, and 2004
Cold Aero Performance of a Two-Dimensional Mixer Ejector Nozzle
Advanced Methods for Aircraft Engine Thrust and Noise Benefits: Nozzle-Inlet Flow Analysis
Mars Flyer Rocket Propulsion Risk Assessment Kaiser Marquardt Testing
Inlet Flow Characteristics During Rapid Maneuvers for an F/A-18A Airplane
High Stability Engine Control (HISTEC) Flight Test Results
F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack
Aerodynamics of Heat Exchangers for High-Altitude Aircraft
Design and Development of an F/a-18 Inlet Distortion Rake: A Cost and Time Saving Solution
Design and Development of an F/A-18 Inlet Distortion Rake: A Cost and Time Saving Solution
Shock-Tunnel Combustor Testing for Hypersonic Vehicles
Aeropropulsion Test and Evaluation Methods