D. L. Maiden

发表

Performance of twin two-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20

F. J. Capone, D. L. Maiden, 1977 .

Performance characteristics of a single-engine fighter model fitted with an in-flight thrust reverser

C. E. Mercer, D. L. Maiden, 1971 .

Effects of an in-flight thrust reverser on the stability and control characteristics of a single-engine fighter airplane model

C. E. Mercer, D. L. Maiden, 1972 .

Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to Mach 2.01

D. L. Maiden, 1975 .

Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at Mach numbers up to 2.01

D. L. Maiden, 1976 .

Atmospheric Ionizing Radiation (AIR): Analysis, Results, and Lessons Learned From the June 1997 ER-2 Campaign

D. L. Maiden, P. Goldhagen, P. Goldhagen, 2003 .

Performance comparison of a lobed-daisy mixer nozzle with a convergent nozzle at subsonic speeds

D. L. Maiden, 1973 .

Atmospheric Ionizing Radiation (AIR) ER-2 Preflight Analysis

D. L. Maiden, W. John, Tai Hsiang, 1998 .