Design handbook for high temperature aerospace antennas.

"Technical report AFAL-TR-65-267"

The structural stability of welds in columbium alloys. Technical documentary report no. ML-TDR-64-210.

Cover title.

Flight evaluation of various phugoid dynamics and 1/Th values for the landing-approach task.

"This is the second in a series of two reports dealing with longitudinal handling qualities in the landing approach." (see also TL/711/L3/C43+)

Study of high-density hypervelocity flows and similitudes

"AEDC-TR-67-72"

Aerothermodynamic consequences of nozzle nonequilibrium

"The research reported herein was...done by the Cornell Aeronautical Laboratory, Inc., for Arnold Engineering Development Center (AEDC) Air Force Systems Command (AFSC), under Program element 62405214, Project 6951, Task 695104."

Endurance tests of rolling contact bearings of conventional and high temperature steels under conditions simulating aircraft gas turbine applications

"Propulsion Laboratory, Contract no. AF 33(600)-22860, Task 3066-30233."

The study of ablation of structural plastic materials

"Preprint copy."

Bibliography on the theory of diffraction and propagation of radio waves

"ASTIA document no. AD 117044."

Approximate solutions for nonequilibrium airflow in hypersonic nozzles,

Contract no. AF40(600)-804. AEDC TN-60-181. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee. Air Research and Development Command, United States Air Force."

A feasibility study of self-learning adaptive flight control for high performance aircraft

"Technical report AFFDL-TR-67-18"

Investigation of the fatigue properties of molybdenum under various conditions of temperature, coatings, and stress concentration

"Materials Central, Contract No. AF 33(616)-5915, Project No. 7350."

A 50-megawatt arc heater: scaling parameters and performance prediction

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

The development of a thermionic converter module suitable for liquid metal heating.

"Project 8173, Task no. 817305-9."

Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16.

Cornell Aeronautical Laboratory, Inc., Buffalo. Report no. AA-1948-Y-3

Bibliography on German guided missiles.

"Report no. F-BB-2-RE."