Add to ORKGAn attempt is made to indicate and briefly discuss only the most significant achievements of the research. The most successful contribution from the contract was the code for two dimensional analysis of airfoils in transonic flow
The input parameters are presented for a computer program which performs calculations for inviscid i...
A comprehensive review of all NASA airfoil research, conducted both in-house and under grant and con...
Numerical optimization was used in conjunction with an inviscid, full potential equation, transonic ...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
Experimental flow investigations on smooth airfoils were done using numerical solutions for transoni...
Major emphasis was on the design of shock free airfoils with applications to general aviation. Unste...
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...
A method for the design of shock free supercritical airfoils, wings, and three dimensional configura...
The five basic elements of the two dimensional airfoil research program at Ames Research Center are ...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
Research in the area of computational, unsteady transonic flows about airfoils and wings, including ...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
"Contract No. AT(30-1)-1480.""October 1969.""Mathematics and Computers."Includes bibliographical ref...
A 20.8 percent-thick airfoil shape was designed to have shockless inviscid flow at a Mach number of ...
The input parameters are presented for a computer program which performs calculations for inviscid i...
A comprehensive review of all NASA airfoil research, conducted both in-house and under grant and con...
Numerical optimization was used in conjunction with an inviscid, full potential equation, transonic ...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
Experimental flow investigations on smooth airfoils were done using numerical solutions for transoni...
Major emphasis was on the design of shock free airfoils with applications to general aviation. Unste...
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...
A method for the design of shock free supercritical airfoils, wings, and three dimensional configura...
The five basic elements of the two dimensional airfoil research program at Ames Research Center are ...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
Research in the area of computational, unsteady transonic flows about airfoils and wings, including ...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
"Contract No. AT(30-1)-1480.""October 1969.""Mathematics and Computers."Includes bibliographical ref...
A 20.8 percent-thick airfoil shape was designed to have shockless inviscid flow at a Mach number of ...
The input parameters are presented for a computer program which performs calculations for inviscid i...
A comprehensive review of all NASA airfoil research, conducted both in-house and under grant and con...
Numerical optimization was used in conjunction with an inviscid, full potential equation, transonic ...