S. J. Miley

发表

Flight Investigations of Tollien-Schlichting Waves on an Aircraft Wing.

K. H. Horstmann, G. Redeker, S. J. Miley, 1990 .

The NASA B737-100 high-lift flight research programme — measurements and computations

C. P. van Dam, L. P. Yip, S. J. Miley, 1995, The Aeronautical Journal (1968).

Propeller propulsion integration, phase 1. [conducted in langley 30 by 60 foot full scale wind tunnel

S. J. Miley, G. Bennett, K. Koenig, 1981 .

Aerodynamics of horizontally-opposed aircraft engine installations

E. J. Cross, J. K. Owens, S. J. Miley, 1977 .

Aerodynamics of Liquid-Cooled Aircraft Engine Installations

S. J. Miley, S. Miley, 1985 .

Flight test method for the determination of reciprocating engine cooling requirements

E. J. Cross, S. J. Miley, D. L. Lawrence, 1981 .

An Investigation of the Aerodynamics and Cooling of a Horizontally-Opposed Engine Installation

E. J. Cross, J. K. Owens, S. J. Miley, 1977 .

Practical flight test method for determining reciprocating engine cooling requirements

S. J. Miley, D. T. Ward, 1984 .

In-Flight Boundary-Layer State Measurements on a High-Lift System: Slat

C. P. van Dam, P. M. H. W. Vijgen, L. P. Yip, 1997 .

Data Report of Flight and Windtunnel Investigations of Tollmien-Schlichting Waves of an Aircraft Wing

K. H. Horstmann, S. J. Miley, S. J. Miley, 1991 .

An experimental investigation of vortex stability, tip shapes, compressibility, and noise for hovering model rotors

J. L. Tangler, S. J. Miley, R. M. Wohlfeld, 1973 .