The preparation of mono- and di-substitution products of trichloro-s-triazine by replacement of chlorine by trialkylsilylphenyl

"Materials Central, Contract no. AF 33(616)-6480, Project no. 7340."

Stability of the boundary layer;

Reproduced from typewritten copy.

Proceedings [held] April 16-19, 1963.

Mode of access: Internet.

Development of a continuous flow electromagnetic alternating current traveling wave accelerator for high-density, hypervelocity wind tunnel applications,

Mode of access: Internet.

Synthesis of flight control systems subject to vehicle parameter variations.

Mode of access: Internet.

Pressure gradient effects on supersonic boundary layer turbulence : final report /

"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."

Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /

"AFAPL-TR-79-2010."

Outer-space environment models for use with space vehicle simulators.

"Project no. 6114, task no. 60806. Prepared under Contract no. AF 33(616)-6858 by W. A. Livingston Jr. of the Cornell Aeronautical Laboratory, Inc."

Technology of missile science.

"Contract no. AF 33(608)-642."

Performance improvement of arc heaters for aerodynamic wind tunnels

Mode of access: Internet.

An investigation of laminar heat transfer to slender cones in the hypersonic shock tunnel

"Contract no. AF-33(616)-6025. Project no. 7064. Task no. 70169. Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, Wright-Patterson Air Force Base."

Helium injection into the boundary layer at an axisymmetric stagnation point

"Contract no. AF 33(616)-7661, Project no. 7064, Task no. 70169."

Reduction of drag due to lift at supersonic speeds

"Aeronautical Research Laboratory, Contract no. AF 33(616)-2170, Project no. 1366."

Experimental studies of high temperature hypersonic diffusers.

"Project No. 1426. Task No. 142612."

Axisymmetric Hall-arc jet wind tunnel driver study

Mode of access: Internet.