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Variable-sweep transition flight experiment (vstfe): stability code development and clean-up glove data analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rozendaal, Roger A. |
| Copyright Year | 1987 |
| Description | The primary objective of the Variable Sweep Transition Flight Experiment (VSTFE) was to establish an improved swept wing transition criterion. The development of the Unified Stability System gave a way of quickly examining disturbance growth for a wide variety of laminar boundary layers. The disturbance growth traces shown are too scattered to define a transition criteria to replace the F-111 data band, which has been used successfully to design NLF gloves. Still, a careful review of the clean-up glove data may yield cases for which the transition location is known more accurately. Liquid crystal photographs of the clean-up glove show much spanwise variation in the transition front for some conditions, and this further complicates the analyses. Several high quality cases are needed in which the transition front is well defined and at a relatively constant chordwise station. |
| File Size | 619143 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900003232 |
| Archival Resource Key | ark:/13960/t0ps2p78z |
| Language | English |
| Publisher Date | 1987-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests Laminar Flow Variable Sweep Wings Tollmien-schlichting Waves Boundary Layer Transition Boundary Layer Stability Blasius Flow Flight Envelopes Cross Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |