Response of a Helicopter Rotor to an Increase in Collective Pitch for the Case of Vertical Flight
Airplane Yaw Perturbations due to Vertical and Side Gusts
Estimation of Leading-Edge Thrust for Supersonic Wings of Arbitrary Planform
Aerodynamic Characteristics of a Finite-Span Flapped Wing Moving near a Solid Wall
Characterization of Attitude Control Propulsion Systems
Launch Vehicle Trajectory Optimization Computer Program, Phase 4 Summary Report
Legacy of the Space Shuttle from an Aerodynamic and Aerothermodynamic Perspective
A Study of Propellant Behavior at Zero Gravity Final Report
Driving Parameters for Distributed and Centralized Air Transportation Architectures
A Calculation of the Lateral Hunting Motion of a Tracked Vehicle
On a Numerical Solution of the Integral Equation of Ducted Propellers with a Tip Clearance
A Numerical Solution of the Unsteady Airfoil with Application to the Vortex Interaction Problem
An Analytical Study for the Design of Advanced Rotor Airfoils
Torsional Oscillation of Helicopter Blades Due to Stall
Hydrological Modeling and Data Assimilation Activities at NASA SPoRT
Quarterly Reports: Railway Technical Research Institute, Volume 13, Number 2, 1972
Surfacing Rescue Container Concept Design for Trident Submarines
Investigation of Velocity Field Behind Low-Flying Wing with Fuselage
A Shock Spectra and Impedance Method to Determine a Bound for Spacecraft Structural Loads
Multidisciplinary Computational Research