Lift Coefficient Predictions for Delta Wing Under Pitching Motions
2002 (English)In: 32nd AIAA Fluid Dynamics Conference Proceedings (2002), USA: AIAA , 2002, AIAA-2002-2969- p.Conference paper (Refereed)
An analytic prediction method is presented to estimate the lift coefficient of delta wings under pitching motions. The method is based on the leading edge suction analogy, with regards to the dynamic effect resulting in the unsteady behaviour. The goal of the method is to provide suitable lift equation for use in simulation in preliminary design.
Place, publisher, year, edition, pages
USA: AIAA , 2002. AIAA-2002-2969- p.
Engineering and Technology
IdentifiersURN: urn:nbn:se:liu:diva-40982DOI: 10.2514/6.2002-2969Local ID: 54814OAI: oai:DiVA.org:liu-40982DiVA: diva2:261832
32nd AIAA Fluid Dynamics Conference. 24 June 2002 - 26 June 2002. St. Louis, Missouri.