Spreading of supersonic jets from axially symmetric nozzles

Mode of access: Internet.

Approximate solutions for nonequilibrium airflow in hypersonic nozzles,

Contract no. AF40(600)-804. AEDC TN-60-181. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee. Air Research and Development Command, United States Air Force."

Hypersonic nozzle design to avoid particle damage.

Caption title.

Aerothermodynamic consequences of nozzle nonequilibrium

"The research reported herein was...done by the Cornell Aeronautical Laboratory, Inc., for Arnold Engineering Development Center (AEDC) Air Force Systems Command (AFSC), under Program element 62405214, Project 6951, Task 695104."

Elements of aerodynamics of supersonic flows.

Bibliography: p. 385-387.

Supersonic inlet diffusers and introduction to internal aerodynamics.

Includes bibliography.

The Secretary's decision on Concorde supersonic transport /

Microfiche. Springfield, Va. : National Technical Information Service, 1976. -- 2 fiche ; 10 x 15 cm. -- AD A022 340.

Solid rocket motor nozzles /

"...written by Russell A. Ellis."

Liquid rocket engine nozzles /

Cover title.

Handbook of supersonic aerodynamics.

Includes bibliographies.

Supersonic aeroelastic effects on static stability and control. Flight Control Laboratory. Contract nos. AF33 (616)-3577 and AF33(616)-6067. ARDC Project no. 8219. Task no. 82158.

pt. 3. Aeroelastic interaction, by V. W. Donato.

The calculation of three-dimensional supersonic flows around spherically-capped smooth bodies and wings

"Work performed for the Air Force Flight Dynamics Laboratory...by the Aerodynamics Research Department of the Northrup Corporation, Aircraft Division."

Effect of thermal stresses on the aeroelastic stability of supersonic wings.

Mode of access: Internet.

Pressure gradient effects on supersonic boundary layer turbulence : final report /

"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."

Reduction of drag due to lift at supersonic speeds

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