Entree d'Air pour un Lanceur Hypersonique (Air Intake for a Hypersonic Launcher)
Seventh European Rotorcraft and Powered Lift Aircraft Forum
Analytical Study of Helicopter Gust Response at High Forward Speeds
L M Controllability During Dps Thrusting - Project APOLLO
Problems of Interpretation of Satellite Weather Data
Radial and Binormal Thrusting Techniques for Maneuvering Satellites in Near Earth Space
Performance evaluation of a urea-selective catalytic reduction system in a marine diesel engine
Quasi-One-Dimensional Modeling of Pulse Detonation Rocket Engines
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
THE NUMERICAL CALCULATION OF PLANE STEADY TRANSONIC FLOWS PAST LIFTING AIRFOILS
Aircraft Noise Source and Computer Programs - User'S Guide
Downwash Investigations on Missile Tails . Abwinduntersuchungen an Leitwerken von Flugkoerpern
Distributed Actuation and Sensing on an Uninhabited Aerial Vehicle
Steady-State Cycle Deck Launcher Developed for Numerical Propulsion System Simulation
Formulation of the Optimal Trajectory for an Air-Breathing Medium Range Air-to-Air Missile
Doppler Observable Modeling for the APOLLO Real-Time Orbit Determination Program
Numerical Techniques for High Incidence Reentry Aerodynamics
Use of Low Constant Thrust to Accomplish Orbital Transfer
Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet Flows with Shock Interactions
Numerical Propulsion System Simulation (NPSS): An Award Winning Propulsion System Simulation Tool
Numerical Integration in a Rigid-Body Trajectory Program
A Mathematical Force and Moment Model of a UH-1H Helicopter for Flight Dynamics Simulations
Analytical Study to Define a Helicopter Stability Derivative Extraction Method, Volume 1
NPSS Model of a Proposed Altitude Test Facility
Advanced Methods for Aircraft Engine Thrust and Noise Benefits: Nozzle-Inlet Flow Analysis
Airport Performance Estimation for Powered Lift Aircraft
Use of Optimization to Predict the Effect of Selected Parameters on Commuter Aircraft Performance
Lessons Learned from Inlet Integration Analysis of NASA's Low Boom Flight Demonstrator
High Power MPD Thruster Development at the NASA Glenn Research Center
The Potential Flow About a Yawed Ellipsoid at Zero Incidence