Unsteady, one-dimensional flow over a plane; the rising hydrograph

Caption title.

Heat-transfer and friction-flow characteristics of cylindrical parallel rods with transverse cylindrical spacers /

Includes bibliographical references (p. 15)

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

Photocopy.

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.

A new method for providing continuous high-temperature air flow for hypersonic research,

"AFOSR-TN-56-236."

Chemical non-equilibrium shock flow,

"Work performed for the Ballistic Systems Divisions, USAF, under Contract no. AF04(647)-617."

Uniformly valid second-order solution for supersonic flow over cruciform surfaces,

"CM-1019."

Illustrated catalogue of the exhibition of Spanish old masters in support of National Gallery funds and for the benefit of the Sociedad de Amigos del Arte Española, Oct. 1913 to Jan. 1914.

Mode of access: Internet.

Report on the operations of the Paper Currency Department in the Lahore circle and on the movement of funds and recource [!] operations of government in the Punjab and North-west frontier province.

Mode of access: Internet.

Federal aid for education. Hearings before the Committee on education and labor, U. S. Senate, 79th Congress, 1st session, on S. 181, a bill to authorize the appropriation of funds to assist the states and territories in more adequately financing their systems of public education during emergency, and in reducing the inequalities of educational opportunities through public elementary and secondary schools...

James E. Murray, chairman.

Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method,

"CM-1034."

Reverse-flow integral methods for second-order supersonic flow theory,

"CM-1033."

Reverse flow and supersonic interference.

"AFOSR TN-58-625. ASTIA doc. no. AD 162 155."

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."

Impact of PL 94-566 on agricultural employers and UI trust funds in selected states.

"Prepared by G. Joachim [i.e. Joachim G.] Elterich and Linda Graham"--Prelim. p.