3D/4D Area Navigation System Design, Development, and Implementation. Volume 1. Main Text
3D and 2.5D Viscous Flow Computations for Axial Flow Turbine Blades
3D CFD Combustion Modeling In Two-Stroke OPOC DISI Engine For Light Aircrafts Applications
3D ENDWALL PROFILING IMPACT ON AXIAL FLOW COMPRESSOR AERODYNAMICS
3D Fatigue Crack Growth Prediction of Web Forging Flaws of a Turbine Disc
3D imaging application in the studies of micro air vehicles
3-Dimensional flow analysis in an intercasing duct with struts
3-Dimensional Study on the Interaction Between Scramjet Engine Modules in Case of Unstart Transition
3D Laser Anemometry in a Rotating Cooling Ribbed U-Channel
3D Non-Planar Crack Growth Prediction in an Engine Compressor Disc
3D Representation of UAV-obstacle Collision Risk under off-nominal conditions
3D Representation of UAV-obstacle Collision Risk Under Off-nominal Conditions
3D velocity measurements within an automotive air handling unit using a single 5-beam LDA probe
3D Visualization of Cooperative Trajectories
4D ATM Cockpit: Set-Up and Initial Evaluation
4D BADA-based Trajectory Generator and 3D Guidance Algorithm
4D BADA-based Trajectory Generator and 3D Guidance Algorithm
5-Year Update Environmental Assessment for CV-22 Beddown
8- by 6-Foot Supersonic Wind Tunnel Compressor Inspected
8 m x 6 m Low Speed Wind Tunnel at the Chinese Aerodynamic Research and Development Center
9- by 15-Foot Low Speed Wind Tunnel Acoustic Improvements Expanded Overview
9-Ft By 7-Ft Supersonic Wind Tunnel Nozzle Improvement Study
15 Pole Connector Between Towing Vehicles and Trailers with 12 Volt Nominal Supply
15 Pole Connector Between Towing Vehicles and Trailers with 12 Volt Nominal Supply
15 Pole Connector Between Towing Vehicles and Trailers with 12 Volt Nominal Supply
21ST Century Air-To-Air Short Range Weapon Requirements
30TH Airlines International Electronics Meeting Proceedings
50 to 100 Ah lithium-ion cells for aircraft and spacecraft applications
50 Years of Gas Turbine Engineering
70 Years of Aeropropulsion Research at NASA Glenn Research Center
70 Years of Aeropropulsion Research at NASA Glenn Research Center
80- to 100-HP Stirling Engine Feasibility Study. Progress Report No. 21, January--March 1977
100 LBS TO Low Earth Orbit (LEO): Small-Payload Launch Options
100 LBS TO Low Earth Orbit (LEO): Small-Payload Launch Options
727 Noise Retrofit Feasibility. Volume III. Upper Goal Flight Testing and Program Summary
727Noise Retrofit Feasibility. Volume I. Lower Goal Design, Fabrication, Ground and Flight Testing
1966 Census of Air Taxi Operators
1975 General Aviation Activity Survey
1988 Model-Year New Motor Vehicle/Engine Certification Summary
1990-1991 Aviation System Capacity Plan