The influence of two-dimensional stream shear on airfoil maximum lift,

"Project 9R-38-01-000, Task 902. Contract DA 44-177-TC-439. U. S. Army Transportation Research Command, Transportation Corps, Fort Eustis, Virginia."

An analysis of nonequilibrium inviscid flow,

"Air Force contract no. AF40(600)-928."

An experimental study of the effect of mass injection at the stagnation point of a blunt body,

"Army Ordnance contract no. DA-04-495-Ord-19."

Tables of two-dimensional oscillating airfoil coefficients for rotary wings.

Mode of access: Internet.

Étude sur l'aviation,

Mode of access: Internet.

Linearized theory of conical supersonic flow with application to triangular wings /

Loose-leaf.

Flight without formula : simple discussions on the mechanics of the aeroplane /

Mode of access: Internet.

Fluid-dynamic drag; practical information on aerodynamic drag and hydrodynamic resistance

Mode of access: Internet.

The resistance of the air and aviation experiments conducted at the Champ-de-Mars laboratory,

Mode of access: Internet.

NASA technical report.

Description based on: R-180; title from cover.

The slow motion of a permanently magnetized sphere in an electrically conducting medium,

"Research supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P.O. 7S4899-R and by the Purdue Research Foundation."

Airborne simulation for the SST.

Cover title.

On the use of impact theory for slender configurations exhibiting flow separation /

Photocopy.

Quasi-three-dimensional supersonic viscid/inviscid interactions including separation effects : final report for period, 1 October 1972- 30 September 1975 /

Bibliography: p. 77-83.

Nonsteady discharge of subcritical flow /

At head of title: Project SQUID, a cooperative program of fundamental research as related to jet propulsion, Office of Naval Research, Department of the Navy. Contract Nonr 1858 (25), NR-098-038.