Z. T. Applin

发表

Flow improvements in the NASA Langley 4- by 7-meter tunnel circuit

Z. T. Applin, 1984 .

Modification to the NASA Langley 4- by 7-meter tunnel for improved rotorcraft aerodynamics and acoustics

Z. T. Applin, 1984 .

HSR High-Lift Technology Overview

Z. T. Applin, 1999 .

Flow improvements in the circuit of the Langley 4- by 7-meter tunnel

Z. T. Applin, 1983 .

Study of several factors affecting crew escape trajectories from the Space Shuttle Orbiter at low-subsonic speeds

G. L. Gentry, G. M. Ware, Z. T. Applin, 1985 .

Status of NASA advanced LFC airfoil high-lift study

Z. T. Applin, 1982 .

Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel

W. L. Sellers, Z. T. Applin, J. K. Molloy, 1984 .

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model

Z. T. Applin, G. Gentry, 1990 .

Stability and Control Results for Advanced Turboprop Aft-Mount Installations

Z. T. Applin, L. J. Williams, Paul L. Coe, 1984 .

The Langley 14- by 22-Foot Subsonic Tunnel: Description, Flow Characteristics, and Guide for Users

Gregory M. Gatlin, Z. T. Applin, P. Frank Quinto, 1990 .