| Model Supports |
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| The rotary balance arm suspends a model in the air stream at angles of attack from 0 to 90 degrees and angles of sideslip between +/-45 degrees while maintaining the relative position of the model reference center. Both top- and aft-mount stings are available. The rig may be rotated in both the clockwise or counterclockwise directions at up to 60 rpm. The system is capable of supporting models weighing up to 15 lb . | ||
![]() Spin Test in 20ft Vertical Spin Tunnel |
![]() Model on swing rig. ![]() Model mounted on rotary balance. |
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| Type of Testing |
Test Request Procedures |
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![]() Dynamically scaled free spin model with parachute. |
Dynamically scaled, free-flying models are used to investigate large angle, high rate phenomena. Aircraft models can be tested for spinning, tumbling, and other out-of-control situations. Spacecraft models can be used for free-fall and dynamic stability characteristics. Tests images are documented on high-resolution color video. The spin recovery characteristics of aircraft are studied by using remote actuation of the aerodynamic control surfaces of the models. Sizing of emergency spin-recovery parachutes systems for flight test aircraft is also available. Nondynamically scaled models can be mounted on a rotary balance apparatus to conduct six-component force and moment testing and surface pressure measurements of models under rotating conditions. Data from these tests are used to calculate the steady spin modes of a configuration, as well as to implement prediction of spins and other high angular rate maneuvers in six degree-of-freedom computer simulations. | The first step of the test process is to submit a test request form. The form can be filled out electronically or printed for mailing at the NASA Langley aero Compass website. A posttest questionnaire is also available at this site. Our customers are encouraged to provide feedback to the facility for our continuous improvement process. |
| Document Version 1.0 |
Trademark Disclaimer: The use of trademarks or names of manufacturers in this report is for accurate reporting and does not constitute an official endorsement, either expressed or implied, of such products or manufacturers by the National Aeronautics and Space Administration. |
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| For more information contact: The 20-Foot Vertical Spin Tunnel Manager -- NASA Langley Research Center -- Hampton, Virginia 23681-2199 phone: 757 ° 864 ° 1194 | fax: 757 ° 864 ° 7722 | e-mail: wte+ fm_20ft@larc. nasa. gov |
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| NASA Official Responsible For Content: Pete Jacobs |
Page Curator: CONITS Development Team | Date Last Updated:11/17/2005 |