FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W3030755001> ?p ?o ?g. }

• W3030755001 endingPage "105883" @default.
• W3030755001 startingPage "105883" @default.
• W3030755001 abstract "Hypersonic waveriders have the potential to significantly reduce travel times on long haul civilian transport routes. The design of hypersonic aircraft is heavily influenced by the aerodynamic efficiency at the cruise Mach number, resulting in less than ideal geometries for subsonic flight. Waverider aerodynamics and stability in the low speed regime is rarely investigated and not well understood, but is crucial for horizontal take-offs and landings. To date, low speed analyses of waverider shapes is confined to static investigations, with no studies on the dynamic behaviour ever completed. This paper presents results from unsteady Reynolds Averaged Navier Stokes simulations modelling pitching and plunging forced oscillations of the low speed propelled variant of the Mach 8 HEXAFLY-INT waverider. Tests were conducted at a speed of 20 m/s, which correlates to a Reynolds number of approximately 1.5×106. Pitching and plunging oscillations were at 1 Hz with an angle of attack amplitude of 1 degree. The vehicle was analysed through an angle of attack range from -5 to 15 degrees in 5 degree increments. Results for the HEXAFLY-INT aircraft at the nominal centre of gravity location, 44.4% of the vehicle length, show that the vehicle is positively damped for all cases tested. Static derivative predictions extracted from the dynamic data showed strong agreement with existing static CFD and wind tunnel results. Further dynamic investigations conducted at a centre of gravity location of 53.1% of the vehicle length, the aft static stability limit, also showed positive damping. For these cases, the derivative magnitudes were lower, which indicates decreased damping compared to the nominal centre of gravity location. The vehicle was generally not sensitive to changes in driving frequency, with oscillation rates ranging from 0.5 to 2 Hz tested. However, during plunging tests, the pitching moment derivative was seen to change by as much as 22%. This is attributed to changes in the leading edge vortices with AoA rate. The results from this study, along with previous work looking at the static aerodynamics, stability and control authority, show the feasibility of moving to the flight test phase, but the aircraft dynamic stability in the lateral-directional planes must first be investigated." @default.
• W3030755001 created "2020-06-05" @default.
• W3030755001 creator A5033125336 @default.
• W3030755001 creator A5035991892 @default.
• W3030755001 creator A5046405453 @default.
• W3030755001 date "2020-08-01" @default.
• W3030755001 modified "2023-10-16" @default.
• W3030755001 title "Low speed longitudinal dynamic stability analysis of a hypersonic waverider using unsteady Reynolds averaged Navier Stokes forced oscillation simulations" @default.
• W3030755001 cites W1980837018 @default.
• W3030755001 cites W2068331296 @default.
• W3030755001 cites W2117630121 @default.
• W3030755001 cites W2161749324 @default.
• W3030755001 cites W2515726757 @default.
• W3030755001 cites W2749407135 @default.
• W3030755001 cites W2803271641 @default.
• W3030755001 cites W2889745879 @default.
• W3030755001 cites W2898245507 @default.
• W3030755001 cites W2922492626 @default.
• W3030755001 cites W2987404626 @default.
• W3030755001 doi "https://doi.org/10.1016/j.ast.2020.105883" @default.
• W3030755001 hasPublicationYear "2020" @default.
• W3030755001 type Work @default.
• W3030755001 sameAs 3030755001 @default.
• W3030755001 citedByCount "15" @default.
• W3030755001 countsByYear W30307550012020 @default.
• W3030755001 countsByYear W30307550012021 @default.
• W3030755001 countsByYear W30307550012022 @default.
• W3030755001 countsByYear W30307550012023 @default.
• W3030755001 crossrefType "journal-article" @default.
• W3030755001 hasAuthorship W3030755001A5033125336 @default.
• W3030755001 hasAuthorship W3030755001A5035991892 @default.
• W3030755001 hasAuthorship W3030755001A5046405453 @default.
• W3030755001 hasConcept C102500504 @default.
• W3030755001 hasConcept C121332964 @default.
• W3030755001 hasConcept C122824865 @default.
• W3030755001 hasConcept C127413603 @default.
• W3030755001 hasConcept C13393347 @default.
• W3030755001 hasConcept C146978453 @default.
• W3030755001 hasConcept C154945302 @default.
• W3030755001 hasConcept C165231844 @default.
• W3030755001 hasConcept C182748727 @default.
• W3030755001 hasConcept C196558001 @default.
• W3030755001 hasConcept C198813307 @default.
• W3030755001 hasConcept C2775924081 @default.
• W3030755001 hasConcept C41008148 @default.
• W3030755001 hasConcept C47446073 @default.
• W3030755001 hasConcept C527307 @default.
• W3030755001 hasConcept C57879066 @default.
• W3030755001 hasConceptScore W3030755001C102500504 @default.
• W3030755001 hasConceptScore W3030755001C121332964 @default.
• W3030755001 hasConceptScore W3030755001C122824865 @default.
• W3030755001 hasConceptScore W3030755001C127413603 @default.
• W3030755001 hasConceptScore W3030755001C13393347 @default.
• W3030755001 hasConceptScore W3030755001C146978453 @default.
• W3030755001 hasConceptScore W3030755001C154945302 @default.
• W3030755001 hasConceptScore W3030755001C165231844 @default.
• W3030755001 hasConceptScore W3030755001C182748727 @default.
• W3030755001 hasConceptScore W3030755001C196558001 @default.
• W3030755001 hasConceptScore W3030755001C198813307 @default.
• W3030755001 hasConceptScore W3030755001C2775924081 @default.
• W3030755001 hasConceptScore W3030755001C41008148 @default.
• W3030755001 hasConceptScore W3030755001C47446073 @default.
• W3030755001 hasConceptScore W3030755001C527307 @default.
• W3030755001 hasConceptScore W3030755001C57879066 @default.
• W3030755001 hasFunder F4320320300 @default.
• W3030755001 hasFunder F4320338362 @default.
• W3030755001 hasLocation W30307550011 @default.
• W3030755001 hasOpenAccess W3030755001 @default.
• W3030755001 hasPrimaryLocation W30307550011 @default.
• W3030755001 hasRelatedWork W1586484240 @default.
• W3030755001 hasRelatedWork W2019724991 @default.
• W3030755001 hasRelatedWork W2029650400 @default.
• W3030755001 hasRelatedWork W2041289796 @default.
• W3030755001 hasRelatedWork W2367376832 @default.
• W3030755001 hasRelatedWork W2387479864 @default.
• W3030755001 hasRelatedWork W2388296807 @default.
• W3030755001 hasRelatedWork W3118446141 @default.
• W3030755001 hasRelatedWork W343959566 @default.
• W3030755001 hasRelatedWork W857097709 @default.
• W3030755001 hasVolume "103" @default.
• W3030755001 isParatext "false" @default.
• W3030755001 isRetracted "false" @default.
• W3030755001 magId "3030755001" @default.
• W3030755001 workType "article" @default.