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."

Hypersonic dynamic stability.

pt. 1. Summary [by] L. A. Marshall.--pt. 2. Conical body experimental program [by] R. B. Hobbs, Jr.--pt. 3. Unsteady flow field program [by] H. Rie, E. A. Linkiewicz [and] F. D. Bosworth.

Consistency and variability in peer ratings

"ASTIA document no. AD 215 483."

Development of partially volatile brazing filler alloys for high-temperature application and resistance to oxidation.

Cover title.

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."

Research and development on advanced graphite materials.

Mode of access: Internet.

Automatic runway profile measuring instrumentation and runway properties.

pt. 1. Equipment.--pt. 2. Equipment trials.--pt. 3. Base surveys.

Hypersonic free flight research.

pt. 1 Instrumentation evaluation and data analysis, by R. W. Bogle and R. J. Magnus.--pt. 2 Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf.

Investigation of feasibility of utilizing available heat resistant materials for hypersonic leading edge applications.

"Volumes I through VIII are unclassified while volume IX is classified secret."

Supersonic aeroelastic effects on static stability and control. Flight Control Laboratory. Contract nos. AF33 (616)-3577 and AF33(616)-6067. ARDC Project no. 8219. Task no. 82158.

pt. 3. Aeroelastic interaction, by V. W. Donato.

Refractory metal constitution diagrams

Mode of access: Internet.

The calculation of three-dimensional supersonic flows around spherically-capped smooth bodies and wings

"Work performed for the Air Force Flight Dynamics Laboratory...by the Aerodynamics Research Department of the Northrup Corporation, Aircraft Division."