Selected topics in fluid mechanics, Summer session 1946 [New York University?]

Reproduced from typewritten copy.

Investigation of the flow over simple bodies at Mach numbers of the order of 20 /

"It is shown that adequate means are available for calculating inviscid direct and induced pressures on simple axisymmetric bodies at zero angle of attack. The extent to which viscous effects can alter these predictions is indicated. It is also shown that inviscid induced pressures can significantly affect the stability of blunt, two-dimensional flat wings at low angles of attack. However, at high angles of attack, the inviscid induced pressure effects are negligible."

An investigation of the exact solutions of the linearized equations for the flow past conical bodies,

Reproduced from type-written copy.

NACA research memorandum.

Description based on: RM no. A6G24 (May 12, 1947); title from cover.

NOL hypervelocity wind tunnel, report.

Caption title.

The turbulent boundary layer with variable Prandtl number.

Mode of access: Internet.

An analytical and experimental study of the ionized flow field about a hemisphere cylinder and its effect on the radiation pattern of a slot antenna

Mode of access: Internet.

Airplane design; a textbook of airplane layout and stress analysis calculations with particular emphasis on economics of design.

"First three editions comprising 2400 copies were published between Dec. 1934 and June 1939."

Recirculation principle for ground effect machine two-dimensional tests.

"Task 9R99-01-005-04. Contract DA 44-177-TC-710."

Experiments in transonic flow,

"Prepared by the California Institute of Technology, Pasadena, California, in June 1947, under AAF contract no. W33-038 ac-1717 (11592), supplemental agreement no. 6."

Validity of air data equations at high altitudes.

Mode of access: Internet.

Research on rotating stall in axial flow compressors.

"January 1959."

Roll-yaw control at high angle of attack by forebody tangential blowing /

"October 1995."

Application of the pressure sensitive paint technique to steady and unsteady flow /

"June 1996."

Wind tunnel tests of thin airfoils oscillating near stall.

"January 1969."