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Technical Evaluation Report, Part A - Vortex Flow and High Angle of Attack
System Design of the Pioneer Venus Spacecraft. Volume 13: Preliminary Development Plans
System Design of the Pioneer Venus Spacecraft. Volume 11: Launch Vehicle Utilization
System Design of the Pioneer Venus Spacecraft. Volume 5: Probe Vehicle Studies
Supplemental Environmental Impact Statement for the Evolved Expendable Launch Vehicle Program
Supersonic Transport Airworthiness Standards. F-102 Flight Research Program
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 and Statistical Analysis of the First AIAA Sonic Boom Prediction Workshop