Research and development on the effects of high pressure and temperature on various elements and binary alloys,

"Materials Central, Contract no. 33(616)-5995. Project no. 7351.

Investigation of lateral stability at stall.

"Aeronautical Research Laboratory. Contract no. AF 33(038)-10480, RDO no. 472-106."

Development of alloys having good high temperature properties through powder metallurgy techniques

"Materials Laboratory, Contract number AF 61(514)-1144, Project no. 7351."

Damping energy dissipated by interfaces in beam and plate supports and in sandwich cores.

"Materials Laboratory, Contract no. AF 33(616)-5426, Project no. 7360."

The effect of configurational additions using viscoelastic interfaces on the damping of a cantilever beam.

"Materials Laboratory, Contract no. AF 33(6169-5449, Project no. 7360."

Response of bars (with internal and boundary damping) to transient and random excitation.

"Materials Laboratory, Contract no. AF 33(616)-5426, Project no. 7360."

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."

Development of columbium-base alloys. Project no. 7351, Task no. 735101.

Cover title.

Cohomology operations and obstructions to extending continuous functions /

"Work supported in part by U.S. Air Force Contract AF 18 (600)-1494."

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."