Laurence K. Loftin

发表

Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil Sections

Laurence K. Loftin, L. K. Loftin, 1947 .

Aeronautical vehicles - 1970 and beyond

Laurence K. Loftin, 1971 .

The Effects of Variations in Reynolds Number between 3000000 and 25000000 upon the Aerodynamic Characteristics of a Number of NACA 6-Series Airfoil Sections

Laurence K. Loftin, William J. Bursnall, 1948 .

Research relating to long-range supersonic cruising aircraft.

Laurence K. Loftin, 1968 .

NASA Aerodynamic Research Applicable to Business Aircraft

Laurence K. Loftin, Marion O. McKinney, 1971 .

Toward a Second-Generation Supersonic Transport

Laurence K. Loftin, 1974 .

The effects of variations in Reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Laurence K. Loftin, William J. Bursnall, 1948 .

Exploratory Investigation at High and Low Subsonic Mach Numbers of Two Experimental 6-percent-thick Airfoil Sections Designed to Have High Maximum Lift Coefficients

Albert E. von Doenhoff, Laurence K. Loftin, L. K. Loftin, 1951 .

Experimental investigation of localized regions of laminar-boundary-layer separation

Laurence K. Loftin, W. J. Bursnall, L. K. Loftin, 1951 .

The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Laurence K. Loftin, William J. Bursnall, 1950 .

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)

Laurence K. Loftin, M. Irene Poteat, 1948 .