C. L. Jaeck

发表

Transpiration Cooling System Development for Reentry Vehicles

V. Deriugin, C. L. Jaeck, R. T. Torgerson, 1968 .

Static and wind tunnel near-field/far-field jet noise measurements from model scale single-flow baseline and suppressor nozzles. Volume 1: Noise source locations and extrapolation of static free-field jet noise data

C. L. Jaeck, 1976 .

Static and wind tunnel near-field/far-field jet noise measurements from model scale single-flow base line and suppressor nozzles. Summary report. [conducted in the Boeing large anechoic test chamber and the NASA-Ames 40by 80-foot wind tunnel]

C. L. Jaeck, 1977 .

Weight sensitivity of a space shuttle orbiter to thermal structural combined loads design criteria.

V. Deriugin, B. E. Clingan, A. L. Brown, 1973 .

Static and wind tunnel near-field/far field jet noise measurements from model scale single-flow baseline and suppressor nozzles. Volume 2: Forward speed effects

C. L. Jaeck, 1976 .

Thermal-structural combined loads design criteria study

V. Deriugin, B. E. Clingan, A. L. Brown, 1972 .

Analysis of pressure and heat transfer tests on surface roughness elements with laminar and turbulent boundary layers Final report

C. L. Jaeck, C. Jaeck, 1966 .