Add to ORKGNumerical simulations for the flow around the F-16XL configuration as a contribution t
The F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment was part of the NASA High-Speed ...
This article present an aeroelastic study of CAWAPI F-16XL aircraft. The structural model for this a...
The nature of nonlinear aerodynamic effects for transonic Limit Cycle Oscillation (LCO) mechanisms a...
In this chapter numerical simulations of the flow around F-16XL are performed as a contribution to t...
The second Cranked-Arrow Wing Aerodynamics Project, International, coordinated project has been unde...
Numerical simulations of the flow around F-16XL are performed as a contribution to the Cranked Arrow...
The investigations presented in this paper are carried out within the NATO RTO AVT-161 Task Group f...
A synthesis is presented of recent numerical predictions for the F-16XL aircraft flowfields and aero...
W pracy przedstawiono wyniki badań aerodynamicznych modelu F-16 w tunelu aerodynamicznym, przy opływ...
This article presents an aeroelastic study of CAWAPI F-16XL aircraft. The structural model of this a...
In the early 1980s, two F-16 airplanes were modified to extend the fuselage length and incorporate a...
A supersonic wind tunnel investigation was conducted in the NASA Langley Unitary Plan Wind Tunnel on...
Comparison of measured and simulated flow features for the full-scale F-16XL aircraft Vergelijking v...
The viewgraphs and discussion on code validation for the simulation of supersonic viscous flow about...
A synthesis is presented of recent numerical predictions for the F-16XL aircraft flow fields and aer...
The F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment was part of the NASA High-Speed ...
This article present an aeroelastic study of CAWAPI F-16XL aircraft. The structural model for this a...
The nature of nonlinear aerodynamic effects for transonic Limit Cycle Oscillation (LCO) mechanisms a...
In this chapter numerical simulations of the flow around F-16XL are performed as a contribution to t...
The second Cranked-Arrow Wing Aerodynamics Project, International, coordinated project has been unde...
Numerical simulations of the flow around F-16XL are performed as a contribution to the Cranked Arrow...
The investigations presented in this paper are carried out within the NATO RTO AVT-161 Task Group f...
A synthesis is presented of recent numerical predictions for the F-16XL aircraft flowfields and aero...
W pracy przedstawiono wyniki badań aerodynamicznych modelu F-16 w tunelu aerodynamicznym, przy opływ...
This article presents an aeroelastic study of CAWAPI F-16XL aircraft. The structural model of this a...
In the early 1980s, two F-16 airplanes were modified to extend the fuselage length and incorporate a...
A supersonic wind tunnel investigation was conducted in the NASA Langley Unitary Plan Wind Tunnel on...
Comparison of measured and simulated flow features for the full-scale F-16XL aircraft Vergelijking v...
The viewgraphs and discussion on code validation for the simulation of supersonic viscous flow about...
A synthesis is presented of recent numerical predictions for the F-16XL aircraft flow fields and aer...
The F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment was part of the NASA High-Speed ...
This article present an aeroelastic study of CAWAPI F-16XL aircraft. The structural model for this a...
The nature of nonlinear aerodynamic effects for transonic Limit Cycle Oscillation (LCO) mechanisms a...