Problems in modeling the complex interacting flow fields in the transonic speed regime are reviewed. The limitations of wind tunnel test capabilities are identified, and options for resolving the deficiency are examined. The evolution of the National Transonic Facility, and the various needs for research investigations to be done there are discussed. The relative priorities that should be given within and across subdisciplines for guidance in planning for the most effective use of the facility are considered
The principal sources of flow unsteadiness in the circuit of a transonic wind tunnel are presented. ...
During the past five years, numerous pioneering archival publications have appeared that have presen...
A second wind tunnel test of the FAST-MAC circulation control model was recently completed in the Na...
Fundamental aerodynamic questions for which high Reynolds number experimental capability is required...
A review is made of the performance of a variety of turbulence models in the evaluation of a particu...
This paper discusses Reynolds number scaling for aerodynamic parameters including force and wing pre...
Advanced transonic configurations, such as the supercritical wing, are inherently more sensitive to ...
The characteristics and capabilities of the two tunnels, that relate to studies in the fields of aer...
A compilation of lectures presented at various Universities over a span of several years is discusse...
Advancements have occurred in transonic numerical simulation that place aerodynamic performance desi...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
The aerodynamic characteristics of two similar models of a lifting body configuration were run in tw...
Papers presented at the Transonic Symposium are compiled. The following subject areas are covered: N...
Numerous computational fluid dynamics (CFD) codes are available that solve any of several variations...
Reynolds number, a measure of the ratio of inertia to viscous forces, is a fundamental similarity pa...
The principal sources of flow unsteadiness in the circuit of a transonic wind tunnel are presented. ...
During the past five years, numerous pioneering archival publications have appeared that have presen...
A second wind tunnel test of the FAST-MAC circulation control model was recently completed in the Na...
Fundamental aerodynamic questions for which high Reynolds number experimental capability is required...
A review is made of the performance of a variety of turbulence models in the evaluation of a particu...
This paper discusses Reynolds number scaling for aerodynamic parameters including force and wing pre...
Advanced transonic configurations, such as the supercritical wing, are inherently more sensitive to ...
The characteristics and capabilities of the two tunnels, that relate to studies in the fields of aer...
A compilation of lectures presented at various Universities over a span of several years is discusse...
Advancements have occurred in transonic numerical simulation that place aerodynamic performance desi...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
The aerodynamic characteristics of two similar models of a lifting body configuration were run in tw...
Papers presented at the Transonic Symposium are compiled. The following subject areas are covered: N...
Numerous computational fluid dynamics (CFD) codes are available that solve any of several variations...
Reynolds number, a measure of the ratio of inertia to viscous forces, is a fundamental similarity pa...
The principal sources of flow unsteadiness in the circuit of a transonic wind tunnel are presented. ...
During the past five years, numerous pioneering archival publications have appeared that have presen...
A second wind tunnel test of the FAST-MAC circulation control model was recently completed in the Na...