48-inch hypersonic shock tunnel; description and capabilities.

Mode of access: Internet.

Six-degree-of-freedom equations of motion for a maneuvering re-entry vehicle

Cover title.

Validity of air data equations at high altitudes.

Mode of access: Internet.

Research on rotating stall in axial flow compressors.

"January 1959."

Roll-yaw control at high angle of attack by forebody tangential blowing /

"October 1995."

Application of the pressure sensitive paint technique to steady and unsteady flow /

"June 1996."

Wind tunnel tests of thin airfoils oscillating near stall.

"January 1969."

NACA conference on some problems of aircraft operation; a compilation of the papers presented.

"Papers presented ... on October 9 and 10, 1950."

Demand bibliography : computational fluid dynamics /

"Sample."

Basic studies of rotating stall and an investigation of flow-instability sensing devices

pt. 1. Basic studies of rotating stall flow mechanisms.--pt. 2. Investigation of flow-instability sensing devices.

Hypersonic dynamic stability.

pt. 1. Summary [by] L. A. Marshall.--pt. 2. Conical body experimental program [by] R. B. Hobbs, Jr.--pt. 3. Unsteady flow field program [by] H. Rie, E. A. Linkiewicz [and] F. D. Bosworth.

Thermal effects on static aeroelastic stability and control.

v. 1. Methods of predicting structural temperatures due to aerodynamic heating, by A. H. Blessing.--v. 2. Aerodynamics, by J. R Batt.--v. 3. Experimental and analytical methods for the determination of thermally-affected wing deflectional behavior, by R. H. Gallagher.--v. 3. sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn.

Hypersonic free flight research.

pt. 1 Instrumentation evaluation and data analysis, by R. W. Bogle and R. J. Magnus.--pt. 2 Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf.

Investigation of feasibility of utilizing available heat resistant materials for hypersonic leading edge applications.

"Volumes I through VIII are unclassified while volume IX is classified secret."

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.