The flow of a supersonic jet from a vessel with plane walls. Iztecheniye sverhzvookovoy strooi iz sosooda s ploskimi stenkami.

Translation of Istechenie sverkhzvukovoĭ strui iz sosuda s ploskimi stenkami (romanized form)

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.

Performance testing of the Tetradyne high speed air jet skimmer /

Mode of access: Internet.

Development and evaluation of a pollution prevention technology for surface cleaning and decontamination : cooperative research and development agreement with Cold Jet, Inc.

Mode of access: Internet.

Elements of aerodynamics of supersonic flows.

Bibliography: p. 385-387.

Supersonic inlet diffusers and introduction to internal aerodynamics.

Includes bibliography.

Gas turbines and jet propulsion, including rocket, hydrogen peroxide, and nuclear power plants: theory and application.

"Portions of this book first published [by the Dept. of Marine Engineering, U. S. Naval Academy] as a part of Combustion engines manual and...of Internal combustion engines."

Curved jet flows. Prepared for U. S. Army Aviation Materiel Laboratories, Fort Eustis, Va. Task 1D121401A14203, Contract DA44-177-AMC-238 (T)

Photocopy.

The finite aspect ratio jet flap.

"Project No. 9-38-01-000 Task 902. Contract No. DA 44-177-TC-439. U.S. Army Transportation Research and Development Command, Transportation Corps, Fort Eustis, Virginia. NSA TRECOM Control No. CRD 1759."

Runway overrun and collision, Platinum Jet Management, LLC, Bombardier Challenger CL-600-1A11, N370V, Teterboro, New Jersey, February 2, 2005 /

"PB2007-910401."

Handbook of supersonic aerodynamics.

Includes bibliographies.

Effects of structural flexibility on entry vehicle control systems. [Prepared for NASA under the cognizance of the Jet Propulsion Laboratory, California Institute of Technology.

Cover title.

Spreading of supersonic jets from axially symmetric nozzles

Mode of access: Internet.

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."