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."

Vaporization of compounds and alloys at high temperature.

Mode of access: Internet.

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.

The Aerothermodynamics of aircraft gas turbine engines /

Photocopy. [Springfield, Va. : National Technical Information Service, 1978]. -- 2 v.

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."

R2D2 : a Fortran program for two-dimensional chemically reacting, hyperthermal, internal flows.

"January 1980."

All semiconductor distributed aerospace processor/memory study /

"August 1973."