Performance improvement of arc heaters for aerodynamic wind tunnels

Mode of access: Internet.

Characteristics of six research wind tunnels of the Ames Aeronautical Laboratory.

Mode of access: Internet.

NOL hypervelocity wind tunnel, report.

Caption title.

Development of an apparatus for wind tunnel dynamic experiments at high-[alpha] /

Cover title.

A study of the overall problems of the true-temperature, hypersonic wind tunnel having semi-continuous operation and the preferred methods of solution.

"Supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P. O. 7S4899-R. Purdue Research Foundation. Research project no. 1717. Project Ae-33.

Development of a continuous flow electromagnetic alternating current traveling wave accelerator for high-density, hypervelocity wind tunnel applications,

Mode of access: Internet.

Axisymmetric Hall-arc jet wind tunnel driver study

Mode of access: Internet.

The upwash correction for an oscillating wing in a wind tunnel.

"Contract no. AF-33(038)-17848, study of dynamic stability model testing."

Instrumentation studies for plasma jet and hypersonic wind tunnel,

"This research was supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P.O. 7S4899-R."

A variable atmosphere hypersonic wind tunnel for similitude studies

Mode of access: Internet.

Development and calibration of an aerodynamic disturbance test facility. Volume I: executive summary. Final report.

Mode of access: Internet.

Development and calibration of an aerodynamic disturbance test facility. Volume II: development of requirements and preliminary design. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

Development and calibration of an aerodynamic disturbance test facility. Volume III: construction, calibration and operation. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

An experimental and analytical investigation of the effect of truck-induced aerodynamic disturbances on passenger car control and performance. Interim report.

Federal Highway Administration, Office of Research, Washington, D.C.

Development of aerodynamic disturbance test procedures. Volume I: executive summary. Final report.

National Highway Traffic Safety Administration, Vehicle Engineering Research Division, Washington, D.C.