Wind Tunnel Tests of 16 Percent Thick Airfoil Section with Spoilers at Different Chordwise Positions
Study of Aerodynamic Technology for Single-Cruise Engine V/STOL Fighter/Attack Aircraft
Multiple Complex Demodulation: A Method for Rhythmic Analysis of Physiological and Biological Data
A General Geometric Theory of Attitude Determination from Directional Sensing
Measurement and Analysis of Granular Soil Beneath Lightweight Robotic Running Gear
First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop, Part 1
Effects of Geometric Characteristics of Interchanges on Truck Safety
Computational and Experimental Efforts in Gravity Probe B Microthruster Analysis
Calculation of the Aerodynamic Behavior of the Tilt Rotor Aeroacoustic Model (TRAM) in the DNW
Test Cases for Flutter of the Benchmark Models Rectangular Wings on the Pitch and Plunge Apparatus
Evaluation of Computer Programs for the Design/Analysis of Highway and Railway Bridges
Effects of Geometric Characteristics of Rural Two-Lane Roads on Safety
Outside Loop Control in Asymmetrical Trimmed Flight Conditions
Lift-to-Drag Ratios of Lifting Bodies at Hypersonic Speeds
Aeroheating Analysis for the Mars Reconnaissance Orbiter with Comparison to Flight Data
NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration
General Models for Lateral Stability Analyses of Railway Freight Vehicles
Some Investigations into Wings with Leading Edge Flaps with and Without Fuselage
Runway Operations Planning: A Two-Stage Heuristic Algorithm
Probability Concepts Applied to Sequential Equipment Operation
The Proposed Large European High-Reynolds Number Transonic Wind Tunnel (LEHRT)
Horizontal Tail Loads in Maneuvering Flight
Effect of Port Corner Geometry on the Internal Performance of a Rotating-Vane-Type Thrust Reverser
Research and Development in Needle and Slit Colloid Thrusters
GEROS: A European Grid Generator for Rotorcraft Simulation Methods
Comprehensive Safety Assessments Sediment Methodology for Innovative Geometric Designs
Analysis of Aerodynamic Data Obtained During Eldo F-5 Flight
Methodologies for Predicting and Testing the Combat Damage on Flight Envelopes
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft