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.

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.

Aircraft aerodynamics (Aerodinamika samoleta) Translation.

Translation of Aerodinamika samoleta, preapred under the auspices of the Liaison Office, Technical Information Center, Wright-Patterson AFB, Ohio.

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."

Unmanned electric propulsion mission capabilities of the SNAP-50/SPUR powerplant /

"Contract AT(30-1)-2789."

Airplane design; a textbook of airplane layout and stress analysis calculations with examples and problems.

"Complementary to ... ʻTechnical aerodynamics' by the same author."--Pref.

Theory of magnetism, magnetic properties of materials and use of magnetic materials in instrumentation

Mode of access: Internet.

Proceedings of the Sixth AFOSR Symposium on Advanced Propulsion Concepts, v. 1.

"Volume II (AFOSR-TR-71-3129) consists of the classified portions of the symposium."

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."

Proceedings of the 3rd Aerospace Mechanisms Symposium, held at the Jet Propulsion Laboratory, Pasadena, California, May 23-24, 1968.

Sponsored by the University of Santa Clara, Lockheed Missiles & Space Company, and the Jet Propulsion Laboratory.

Determination of the masses of the Moon and Venus and the astronomical unit from radio tracking data of the Mariner II spacecraft

"Prepared under contract no. NAS 7-100, National Aeronautics and Space Administration."

Bibliographical review of panel flutter and effects of aerodynamic noise

"Materials Laboratory, Contract no. AF 33(616)-5426, Project no. 7360."

Development of a continuous flow electromagnetic alternating current traveling wave accelerator for high-density, hypervelocity wind tunnel applications,

Mode of access: Internet.

Theoretical and experimental studies of airfoil characteristics in nonuniform sheared flow.

At head of title: Task 1P125901A142. Contract DA 44-177-AMC-70 (T). USAAML technical report 65-17.

A theory of wing-propulsion combinations in slow flight.

"Project No. 9-38-01-00 Task 902. Contract No. DA 44177-TC-439. U. S. Army Transportation Research and Development Command, Transportation Corps, Fort Eustis, Virginia."