The objective of this project is to define torque values for bolts and screws when loading is not a concern. Fasteners require a certain torque to fulfill its function and prevent failure. NASA Glenn Research Center did not have a set of fastener torque tables for non-critical applications without loads, usually referring to hand-tight or wrench-tight torqueing. The project is based on two formulas, torque and pullout load. Torque values are calculated giving way to preliminary data tables. Testing is done to various bolts and metal plates, torqueing them until the point of failure. Around 640 torque tables were developed for UNC, UNF, and M fasteners. Different lengths of thread engagement were analyzed for the 5 most common materials used...
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An investigation of the aeroheating environment of the Project Orion Crew Entry Vehicle has been per...
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NASA's NextGen Concepts and Technology Development (CTD) Project focuses on capabilities to improve ...
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Over the last two years a number of workshops or similar meetings have been held under the auspice o...
This paper presents an overview of the fifth revision to an algorithm specifically designed to suppo...
Aeroheating characteristics of the X-33 Rev-F configuration have been experimentally examined in the...
The System-Oriented Runway Management (SORM) concept was developed as part of the Airspace Systems P...
This year end progress report summarizes our engineering study of a large, VTOL civil transport that...
The Badhwar-O'Neill (BON) model has been used for some time to describe the galactic cosmic ray (GCR...
The Tool for Turbine Engine Closed-Loop Transient Analysis (TTECTrA ver2) is a control design tool t...
The use of Computational Fluid Dynamics (CFD) is gaining momentum within the aeronautical community....
This paper presents an overview of the sixth revision to an algorithm specifically designed to suppo...
An investigation of the aeroheating environment of the Project Orion Crew Entry Vehicle has been per...
This paper presents an overview of the seventh revision to an algorithm specifically designed to sup...
Wake vortex spacing standards constrict the terminal area throughput and impose severe constraints o...
This document describes an algorithm for the generation of a four dimensional trajectory. Input data...
NASA's NextGen Concepts and Technology Development (CTD) Project focuses on capabilities to improve ...
This document describes an algorithm for the generation of a four dimensional aircraft trajectory. I...
Over the last two years a number of workshops or similar meetings have been held under the auspice o...
This paper presents an overview of the fifth revision to an algorithm specifically designed to suppo...
Aeroheating characteristics of the X-33 Rev-F configuration have been experimentally examined in the...
The System-Oriented Runway Management (SORM) concept was developed as part of the Airspace Systems P...
This year end progress report summarizes our engineering study of a large, VTOL civil transport that...
The Badhwar-O'Neill (BON) model has been used for some time to describe the galactic cosmic ray (GCR...
The Tool for Turbine Engine Closed-Loop Transient Analysis (TTECTrA ver2) is a control design tool t...
The use of Computational Fluid Dynamics (CFD) is gaining momentum within the aeronautical community....