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Delta
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Supplemental Environmental Impact Statement for the Evolved Expendable Launch Vehicle Program
Supersonic Transport Airworthiness Standards. F-102 Flight Research Program
Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization
Supersonic Flutter Derivatives for a Series of Swept and Cropped delta Wings
Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg
Supersonic Aerodynamic Characteristics of an Advanced F-16 Derivative Aircraft Configuration
Summary of the 2008 NASA Fundamental Aeronautics Program Sonic Boom Prediction Workshop
Summary and Statistical Analysis of the First AIAA Sonic Boom Prediction Workshop
Summary and Statistical Analysis of the First AIAA Sonic Boom Prediction Workshop
Submerged Inlet Performance Enhancement Using a Unique Bump-Shaped Vortex Generator
Sub- and Transonic Vortex Breakdown Flight Condition Simulations of the F-16XL Aircraft
Study on the orbital maneuvering capability of H-2A kick stage
Study of Movement and Seepage Along Levees Using DInSAR and the UAVSAR Instrument
Study of Aerodynamic Technology for Single-Cruise-Engine V/STOL Fighter/Attack Aircraft
Structural Dynamics and Data Analysis
Structural Design for a Neptune Aerocapture Mission
Stress-Strain Analysis of the Circular Orthotropic Plate Under Circumferential Loading
Stochastic Expansions Including Data on the Unit Circle
Sting Influence on Vortex Breakdown on a 65 Degree Delta Wing in Transonic Flow
Static Tests of the J97 Powered, External Augmenter V/STOL Wind Tunnel Model
StarBooster Demonstrator Cluster Configuration Analysis/Verification Program
Stability derivatives of triangular wings at supersonic speeds
Stability Derivatives of Low-Aspect-Ratio Triangular Wings at Subsonic and Supersonic Speeds
Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data
Stability control and energy saving for propulsion of a biomimetic autonomous underwater vehicle
Spanwise Wing Loads on the Space Shuttle Orbiter during Roll Maneuver
Spanwise loading for wings and control surfaces of low aspect ratio
Space Transportation Infrastructure Supported By Propellant Depots