C. A. Trexler

Wind-tunnel tests on a 3-dimensional fixed-geometry scramjet inlet at M = 2.30 to 4.60

J. N. Mueller, C. A. Trexler, S. W. Souders, 1977 .

Design and performance at a local Mach number of 6 of an inlet for an integrated Scramjet concept. [wind tunnel models - aircraft design

C. A. Trexler, S. W. Souders, 1975 .

Flameholding characteristics of a swept-strut H2 fuel-injector for scramjet applications

C. R. Mcclinton, C. A. Trexler, G. B. Northam, 1980 .

Design and performance at a local Mach number of 6 of an inlet for an integrated Scramjet concept

C. A. Trexler, S. W. Souders, 2013 .

Inlet performance of the integrated Langley scramjet module

C. A. Trexler, 1975 .

Instant-replay data system for combustion tests

C. A. Trexler, 1980 .