Manual of surface electromyography

"Republication of a report originally published by the US Army in 1952, under Contract no. DA-49-007-MD-70"

Heat transfer by combined conduction and radiation through a radiating gas.

Thesis (M. S.)--Air Force Institute of Technology.

Low-density research in the hypersonic shock tunnel

"The experimental study reported here has been performed under the sponsorship of the Fluid Dynamics Branch, Aeronautical Research laboratories of the U.S. Air Force Air Research and Development Command, Contract no. AF 33(616)-6025."

OAR index of current research results.

Cumulations issued with title: OAR index of research results.

Thermophysical properties of solid materials

"Materials Central, Contract No. AF 33(616)-5212, Project No. 7381."

Project Neos; a general study of processes for the realization of design configurations in materials

"Cornell Aeronautical Laboratory. Contract: AF 33(600)-42921. ASD project NR 7-867."

Project Neos; a generalized study of processes for the realization of esign configurations in materials. [Final] technical documentary report no. ML-TDR-64-311. MTD project no.7-867.

Mode of access: Internet.

Factors affecting thermal shock resistance of polyphase ceramic bodies

Mode of access: Internet.

Oxidation of tungsten and tungsten based alloys

Part 2 has imprint (on cover): Aeronautical Systems Division, Air Force Systems Command, U. S. Air Force, Wright-Patterson Air Force Base, Ohio.

Investigation of thermal effects on structural fatigue. Flight Dynamics Laboratory. Contract no. AF 33(616)-6571. Project no. 1367. Task 14025.

Mode of access: Internet.

Energy conversion systems reference handbook. [EOS report 390-final]

Contract nr. AF 33(616)-6791. Project nr. 4769. Task nr. 61048."

Consistency and variability in peer ratings

"ASTIA document no. AD 215 483."

Development of new sound absorbing materials for noise suppressors.

"Materials Laboratory, Contract no. AF33(616)-5060, Project no. 7231."

Thermal effects on static aeroelastic stability and control.

v. 1. Methods of predicting structural temperatures due to aerodynamic heating, by A. H. Blessing.--v. 2. Aerodynamics, by J. R Batt.--v. 3. Experimental and analytical methods for the determination of thermally-affected wing deflectional behavior, by R. H. Gallagher.--v. 3. sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn.

Development of the Airman qualifying examination, forms D and E. Project 7717, Task 87005.

"ASTIA document no. AD 151045."