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.

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+)

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

"Technical report AFFDL-TR-67-18"

Synthesis of flight control systems subject to vehicle parameter variations.

Mode of access: Internet.

The unsteady flow field about a right circular cone in unsteady flight.

"These studies were conducted by the General Electric Company, Reentry Systems Department, for the Stability and Control Section of the Flight Dynamics Laboratory of the Air Force Research and Technology Division."

A survey of the literature on the size effect on material strength /

"Final report for period 1 August 1972 to 30 September 1976."

Investigation of current-voltage and flow characteristics of an electric discharge across the exit of the AFFDL 1-Mw arc air heater

"Sponsored by the Air Force Flight Dynamics Laboratory ... under Contract AF 33(615)-1835."

Relative transition probability and pressure broadening parameters of copper atomic lines /

Inserted Report documentation page designates D. W. Boyer ... [et al.] as "authors."

A study of matrix analysis methods for inelastic structures. Project no. 1467, Task no. 146701, prepared under Contract no. AF 33 (657)-8717 by Massachusetts Institute of Technology, Aeroelastic and Structures Research Laboratory.

Cover title.

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.

Automatic runway profile measuring instrumentation and runway properties.

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

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."

USAF damage tolerant design handbook : guidelines for the analysis and design of damage tolerant aircraft structures : final report for period September 1980 to March 1984 /

"May 1984."

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

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