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Iterative method
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Flutter Prediction for Aircraft Conceptual Design
NASA Advanced Concepts Office, Earth-To-Orbit Team Design Process and Tools
Computations on Wings With Full-Span Oscillating Control Surfaces Using Navier-Stokes Equations
Peak Seeking Control for Reduced Fuel Consumption with Preliminary Flight Test Results
NASA Lightning Nitrogen Oxides Model (LNOM): Recent Updates and Applications
Orbiter Trajectory Analysis for a Two-Stage Reusable Launch Vehicle
Shuttle Return-to-Flight IH-108 Aerothermal Test at CUBRC - Flow Field Calibration and CFD
Altair Descent and Ascent Reference Trajectory Design and Initial Dispersion Analyses
Conceptual Aerospace Vehicle Structural System Modeling, Analysis and Design Process
Aerospace Applications of Optimization under Uncertainty
Developing Conceptual Hypersonic Airbreathing Engines Using Design of Experiments Methods
Design and Analysis Techniques for JPL Mobile Antenna Developments
Aerodynamic Aircraft Design Methods and Their Notable Applications: Survey of the Activity in Japan
Aerodynamic Design Techniques at DLR Institute for Design Aerodynamics
One Point and Multi-Point Design Optimization for Airplane and Helicopter Application
Application of Active Controls Technology to a Generic Hypersonic Aircraft Configuration
Lander Program Manual: A Lunar Ascent and Descent Simulation
Space Station Needs, Attributes, and Architectural Options: Space Station Program Cost Analysis
Specification for a Program for an Interative Aeroelastic Solution (PIAS)
A Generalized Modal Shock Spectra Method for Spacecraft Loads Analysis
Design of a Symmetrical Section with Specified Pressure Distribution
Rapid Optimization of Multiple-Burn Rocket Flights, 8 March 1968 - 8 March 1969
On Some Possible Simplifications and Changes in Hansen'S Lunar Theory
Some Recent Results in Aerospace Vehicle Trajectory Optimization Techniques
The Solution of a Satellite Re-Entry Problem by a Gradient Technique