Reduction of drag due to lift at supersonic speeds

"Aeronautical Research Laboratory, Contract no. AF 33(616)-2170, Project no. 1366."

Shock tunnel studies of high-enthalpy ionized airflows,

"AFOSR 3025."

Experimental studies of high temperature hypersonic diffusers.

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

Shock-bounded, self-similar flows with volumetric mass, momentum, and energy addition.

"DCAS-TDR-62-135. Report no. TDR-69 (2230-01)TR-2. Contract no. AF 04(695)-69."

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.

Das Elsass, Volks- und Kulturfragen : die Natürliche Einheit und der kulturelle Zusammenhang der oberrheinischen und süddeutschen Lande /

Leaves of plates (18) numbered as part of pagination sequence.

Frankreichs Schande; eine Lehre aus Frankreichs sittlichem Zusammenbruch,

"Quellenverzeichnis": p. 97-98.

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.

Gesetzsammlung für das Herzogthum Oldenburg.

Mode of access: Internet.