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Browsing AIAA - American Institute of Aeronautics and Astronautics by Issue Date
Now showing items 21-40 of 70
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AIAA G-077
Abstract: The fundamental strategy of V&V is the assessment of error and uncertainty in the computational simulation. The required methodology is a complex process because it must assess errors and uncertainties originating in all ... -
AIAA R-092-2
Abstract: Introduction
The purpose of this recommended practice document is to provide the reader with increased knowledge about planning and executing highly successful wind tunnel tests. First, an overview of ... -
AIAA R-092-1
Abstract: Introduction
Wind tunnel testing is a critical component in the development of aerodynamic vehicles and associated technologies. While the time and expense of wind tunnel testing is significant, it is ... -
AIAA R-091
Abstract: This document provides a recommended method for calibration of internal strain-gage balances used in wind tunnel testing. The practices include terminology, axis system definition, balance calibration methods, matrix, and ... -
AIAA R-093
Abstract: Executive summary
The purposes of this document are (1) to provide an overview of the calibration of subsonic and transonic wind tunnels and (2) to provide a basis for commonality within the wind tunnel ... -
AIAA G-045
Abstract: Abstract
This AIAA Guide supplements the methodology for assessment of experimental uncertainties and techniques for evaluating experimental error sources provided in AIAA Standard S-071A-1999, "Assessment ... -
AIAA G-095
Abstract: Purpose
The purpose of this Guide is to provide a practical set of guidelines for safe hydrogen use. The information presented in this Guide is intended as a reference to hydrogen design and practice ... -
AIAA SP-108
Abstract: This document provides recommended design practices for conceptual engineering studies of nuclear fusion space propulsion systems. Discussion and recommendations are included on key topics including design reference missions, ... -
AIAA S-096
Abstract: This document establishes a top level certification standard for the design, analysis, material selection and characterization, fabrication, test and inspection of the flywheel rotor assembly (FRA) in a flywheel used for ... -
AIAA S-114
Abstract: This standard specifies general requirements for the design, manufacture, quality control, testing, and storage of moving mechanical assemblies (MMAs) to be used on space and launch vehicles. This standard is applicable ... -
AIAA R-101A
Abstract: Abstract
The CFD General Notation System (CGNS) is a standard for recording and recovering computer data associated with the numerical solution of the equations of fluid dynamics. The intent is to ... -
AIAA S-110
Abstract: This document establishes a standard for the design, analysis, material selection and characterization, fabrication, test, and inspection of structural items in space systems, including payloads, spacecraft, upper-stages, ... -
AIAA S-113
Abstract: This standard establishes criteria for design, manufacture, and performance certification of explosive systems and explosive devices commonly used on launch, upper stage, and space vehicle systems. The requirements contained ... -
AIAA G-118
Abstract: The purpose of this Guide is to assist development and maintenance projects (teams and individuals) that have to address the use of, or consideration of, COTS products within large, complex systems, including but not limited ... -
AIAA S-081A
Abstract: This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of composite overwrapped pressure vessels (COPVs) containing a metallic liner. These vessels are used ... -
AIAA S-120
Abstract: This standard defines terminology and establishes uniform processes, procedures, and systematic methods for the management, control, monitoring, determination, verification, and documentation of mass properties during the ... -
AIAA S-122
Abstract: This document, when followed in its entirety, will yield a robust EPS design suitable for very high-reliability space missions. This document specifies general design practices and sets minimum verification and validation ...