A nonintrusive method of quantifying flow visualization data in vortex flow fields /
along with the flow visualization scheme was utilized to
| Main Author: | |
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| Format: | Thesis eBook |
| Language: | English |
| Published: |
[Place of publication not identified] :
[publisher not identified] ;
1994.
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| Subjects: | |
| Online Access: | Link to OAKTrust copy |
| Summary: | along with the flow visualization scheme was utilized to both translational and rotational motion to simulate both created by leading edge extensions and the forebody. With full scale mockup of the HARV demonstrated that the location in flight. A relative motion approach using fixed targets of a target could be determined within one inch of its true of the flow but also a quantitative measure to be used to other similar flight test aircraft have been using smoke flow position or less that 1% of the HARV length. remove unwanted motion. The relative motion algorithm was removing both motions with only a slight loss of accuracy. A test. One of the major drawbacks to employing video imaging tested using a laboratory test setup where cameras underwent the advent of video measurement techniques, this type of flow The High Angle of Attack Research Vehicle (HARV) as well as validate computational fluid dynamic codes and wind tunnel visualization can not only provide a qualitative assessment visualization techniques to characterize the vortex flow was the introduction of false motion due to camera movement wing bending and torsion. The method was effective in |
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| Item Description: | "Major subject: Aerospace Engineering". Includes one 3.5" IBM format computer disk." Vita. |
| Physical Description: | xiii, 73 leaves : illustrations ; 28 cm. + 1 computer disk. Also available online. |
| Format: | System requirements for accompanying disk: IBM PC. |
| Bibliography: | Includes bibliographical references. |