Aeropropulsion facilities at the NASA Lewis Research Center

"B-0712"--P. 33.

The method of characteristics in compressible flow.

Reproduced from typewritten copy.

A study of finite-difference methods as applied to hypersonic viscous shock-layer equations

"Contract no. Nonr 2653(00)."

High velocity jet noise source location and reduction.

"February 22, 1977."

Comparison of the Ohio State University and Penn State University skid system water nozzle /

Mode of access: Internet.

Proceedings of the SCAR Conference, held at Langley Research Center, Hampton, Virginia, November, 9-12, 1976. --

Includes bibliographical references.

Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 /

Prepared at Langley Research Center.

Vector polar method for shock interactions with area disturbances /

"AFOSR TN 59-701. Contract no. AF49(638)-166. I. E. R. project no. 96895."

Drag due to lift of a not-so-slender configuration; application of theory.

"Contract no. AF 33(616)-2933."

Investigations in Soviet hypervelocity testing technique; comprehensive report

"Based on Soviet-satellite open sources published 1924-1965."

Airborne simulation for the SST.

Cover title.

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

Photocopy.

Outflow of a jet of compressed air into moving air.

"A translation."

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.

Investigation of small surface protuberances upstream of turbulent boundary layer separation produced by a skewed shock wave at Mach 3 /

"Interim report for period January 1976-February 1976."