Add to ORKGThe objective of the Subsonic/Transonic Stall Flutter Program was to obtain detailed measurements of...
Comparisons of calculated and experimental transonic unsteady pressures and airloads for four of the...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
An attempt is made to indicate and briefly discuss only the most significant achievements of the res...
Experimental flow investigations on smooth airfoils were done using numerical solutions for transoni...
A series of experiments was conducted on flow fields about two airfoil models whose sections are sli...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
Research in the area of computational, unsteady transonic flows about airfoils and wings, including ...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
A fast computer program was developed to eliminate the shocks by slightly altering portions of the c...
Schlieren photographs have been compiled of the two-dimensional flow at transonic speeds past 37 air...
A method for the design of shock free supercritical airfoils, wings, and three dimensional configura...
Results of computer code time dependent solutions of the two dimensional compressible Navier-Stokes ...
A two-dimensional theory is considered for the unsteady flow disturbances caused by aeroelastic defo...
The objective of the Subsonic/Transonic Stall Flutter Program was to obtain detailed measurements of...
Comparisons of calculated and experimental transonic unsteady pressures and airloads for four of the...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
An attempt is made to indicate and briefly discuss only the most significant achievements of the res...
Experimental flow investigations on smooth airfoils were done using numerical solutions for transoni...
A series of experiments was conducted on flow fields about two airfoil models whose sections are sli...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
Research in the area of computational, unsteady transonic flows about airfoils and wings, including ...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
A fast computer program was developed to eliminate the shocks by slightly altering portions of the c...
Schlieren photographs have been compiled of the two-dimensional flow at transonic speeds past 37 air...
A method for the design of shock free supercritical airfoils, wings, and three dimensional configura...
Results of computer code time dependent solutions of the two dimensional compressible Navier-Stokes ...
A two-dimensional theory is considered for the unsteady flow disturbances caused by aeroelastic defo...
The objective of the Subsonic/Transonic Stall Flutter Program was to obtain detailed measurements of...
Comparisons of calculated and experimental transonic unsteady pressures and airloads for four of the...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...