Computation of wind tunnel wall effects for complex models using a low-order panel method
Explore this paper's citation graph
- Type
- article
- Published
- 1994-02-01
- Cited by
- 1
- References
- 9
- Access
- Open access
- OpenAlex
- https://openalex.org/W73425784
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:52888766
Keywords
Wind tunnel, Lift coefficient, Lift (data mining), Aerodynamics, Pressure coefficient
References
- Potential Flow Theory and Operation Guide for the Panel Code PMARC
- Low-Speed Wind Tunnel Testing
- Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft
- Development and validation of an advanced low-order panel method
- Propulsion-induced aerodynamics of an ejector-configured STOVL fighter aircraft
- Exact solution for wind tunnel interference using the panel method
- Numerical Simulation of the Wind Tunnel Environment by a Panel Method
Cited by
Related papers
- Wind-Tunnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 Degree Swept-Wing Airplane
- Comparative Flight and Full-Scale Wind-Tunnel Measurements of the Maximum Lift of an Airplane
- Experiments with an adaptable-wall wind tunnel for large lift
- Flight Test and Wind Tunnel Performance Characteristics of the X-24A lifting Body. Volume I
- Longitudinal Stability and Control Characteristics of a Semispan Wind-Tunnel Model of the XF7U-1 Airplane and a Comparison with Complete-Model Wind-Tunnel Tests and Semispan-Model Wing-Flow Tests