WFRF:(Tomac M.)
Sökning: WFRF:(Tomac M.) > Hybrid RANS-LES sim...
LIBRIS Formathandbok (Information om MARC21)
| Fältnamn | Indikatorer | Metadata |
|---|---|---|
| 000 | 03080naa a2200529 4500 | |
| 001 | oai:DiVA.org:kth-187532 | |
| 003 | SwePub | |
| 008 | 160525s2015 | |||||||||||000 ||eng| | |
| 024 | 7 | a https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-1875322 URI |
| 024 | 7 | a https://doi.org/10.2514/6.2015-28742 DOI |
| 040 | a (SwePub)kth | |
| 041 | a engb eng | |
| 042 | 9 SwePub | |
| 072 | 7 | a ref2 swepub-contenttype |
| 072 | 7 | a kon2 swepub-publicationtype |
| 100 | 1 | a Rizzi, Arthuru KTH,Farkost och flyg4 aut0 (Swepub:kth)u1ubzhon |
| 245 | 1 0 | a Hybrid RANS-LES simulations of F-16XL aircraft in low-speed high-alpha flight |
| 264 | c 2015-06-19 | |
| 264 | 1 | a Reston, Virginia :b American Institute of Aeronautics and Astronautics,c 2015 |
| 338 | a print2 rdacarrier | |
| 500 | a QC 20160614. QC 20200701 | |
| 520 | a This article presents the comparisons of the results of the CFD study around the F-16XL CAWAPI configuration for flight condition FC25: M∞ = 0:24, α = 19:8°, β = 0°, Re = 32:2M. Previous work has established this case of high angle of attack flight as an outlier in the sense that the computed pressure distributions compared less favorably with those measured in flight tests than did similar comparisons for cases at lower angle of attack. One reason suggested for the discrepancy was that the flow over the outer wing panel was unsteady, possibly including vortex breakdown. This paper presents results computed time accurately with physical modeling that can capture such unsteady flow phenomena. The physical modeling employed is an innovative hybrid RANS-LES model termed HYB0. The simulations obtained are compared with those measured during flight testing of the vehicle as well as with results computed with RANS and URANS physical modeling. Although differences are found among all the results compared, they are not exceeding large. Further analysis of the results are presented, and conclusions are drawn. | |
| 650 | 7 | a TEKNIK OCH TEKNOLOGIERx Maskinteknik0 (SwePub)2032 hsv//swe |
| 650 | 7 | a ENGINEERING AND TECHNOLOGYx Mechanical Engineering0 (SwePub)2032 hsv//eng |
| 653 | a Aerodynamics | |
| 653 | a Angle of attack | |
| 653 | a Angle of attack indicators | |
| 653 | a Computational fluid dynamics | |
| 653 | a Fighter aircraft | |
| 653 | a Flight simulators | |
| 653 | a Navier Stokes equations | |
| 653 | a Research aircraft | |
| 653 | a F-16XL aircraft | |
| 653 | a Flight conditions | |
| 653 | a High angle of attack | |
| 653 | a Hybrid RANS-LES | |
| 653 | a In-flight tests | |
| 653 | a Physical model | |
| 653 | a Unsteady flow phenomenon | |
| 653 | a Vortex breakdown | |
| 653 | a Supersonic aircraft | |
| 700 | 1 | a Tomac, M.4 aut |
| 700 | 1 | a Jirásek, A.4 aut |
| 710 | 2 | a KTHb Farkost och flyg4 org |
| 773 | 0 | t 33rd AIAA Applied Aerodynamics Conferenced Reston, Virginia : American Institute of Aeronautics and Astronauticsz 9781624103636 |
| 856 | 4 8 | u https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-187532 |
| 856 | 4 8 | u https://doi.org/10.2514/6.2015-2874 |
Hitta via bibliotek
- 33rd AIAA Applied Aerodynamics Conference (Sök värdpublikationen i LIBRIS)
Till lärosätets databas
Hitta mer i SwePub
- Av författaren/redakt...
- Rizzi, Arthur
- Tomac, M.
- Jirásek, A.
- Om ämnet
-
- TEKNIK OCH TEKNOLOGIER
- TEKNIK OCH TEKNO ...
- och Maskinteknik
- Artiklar i publikationen
- 33rd AIAA Applie ...
- Av lärosätet
- Kungliga Tekniska Högskolan
Sök utanför SwePub
- Sök vidare i:
- Google Book Search
- Google Scholar
Kungliga biblioteket hanterar dina personuppgifter i enlighet med EU:s dataskyddsförordning (2018), GDPR. Läs mer om hur det funkar här.
Så här hanterar KB dina uppgifter vid användning av denna tjänst.
- Copyright © LIBRIS - Nationella bibliotekssystem
- LIBRIS.kb.se
