Direct and general support maintenance manual : boat, bridge erection, twin jet, aluminum hull, model USCSBMK 1 (1940-01-105-5728).

Includes index.

Operator and organizational maintenance manual (including repair parts and special tools list) : cleaner, steam pressure, jet, trailer mounted, kerosene or light diesel oil fired, electric motor, 1 hp, 115 V, AC/DC, 60 C, SGLE-PH (Geranco Manufacturing Corporation, model GS-400) (4940-865-4738).

"June 1967."

Operator's manual : generator, smoke, mechanical, pulse jet, M3A4 (1040-01-143-9506).

"September 1985."

Organizational and direct support maintenance repair parts and special tools lists for generator, smoke, mechanical, pulse jet, M3A4 (1040-01-143-9506).

"June 1989."

Organizational and direct support maintenance manual [microform] : generator, smoke, mechanical, pulse jet, M3A4 (1040-01-143-9506).

"October 1985."

Operator's manual : boat, bridge erection, twin jet, aluminum hull, model USCSBMK 1 (1940-01-105-5728).

Includes index.

Material presented at the NACA Conference on Supersonic Aerodynamics at Ames Aeronautical Laboratory on June 4, 1946, National Advisory Committee for Aeronautics.

Includes bibliography.

Supersonic aerodynamics and rocket propulsion,

Includes bibliographical references.

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

Bibliography: p. 77-83.

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.

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

"CM-1019."

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."

Pressure distribution on a body a revolution in supersonic flight, by Robert R. Reynolds.

"This report appears as an appendix to the National Applied Mathematics Laboratories Quarterly report of projects and publications, January through March 1952."