National Technical Reports Library

The National Technical Information Service acquires, indexes, abstracts, and archives the largest collection of U.S. government-sponsored technical reports in existence. The NTRL offers online, free and open access to these authenticated government technical reports. Technical reports and documents in its repository may be available online for free either from the issuing federal agency, the U.S. Government Publishing Office’s Federal Digital System website, or through search engines.

Details

ADA147197

Publication Date	1984
Page Count	154
Abstract	Contents: Transonic Wing and Far Field Test Data on a High Aspect Ratio Transport Wing for Three Dimensional Computational Method Evaluation; Transonic Wing and Far Field Test Data on a Moderate Aspect Ratio Wing for Three Dimensional Computational Method Evaluation; Pressure Distributions Measured on Research Wing M100 Mounted on an Axisymmetric Body; Pressure Distribution Measured on Research Wing M86 Mounted on an Axisymmetric Body; and Pressure Distribution on a Swept Wing Aircraft in Flight.
Keywords	Aerodynamic configurations Aerodynamic characteristics Data bases Experimental data Swept wings Supercritical wings Aspect ratio Far field Pressure distribution Transonic characteristics Flight testing Wind tunnel models Two dimensional flow Three dimensional flow Supersonic flow Mathematical models Wing body configurations Great Britain Sweden United States Foreign technology NATO furnished
Source Agency	Non Paid ADAS
NTIS Subject Category	51A - Aerodynamics
Corporate Authors	Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine (France).
Supplemental Notes	Addendum to report dated May 79, AD-A073 982.
Document Type	Technical Report
Title Note	Advisory rept.
NTIS Issue Number	198503

Experimental Data Base for Computers Program Assessment. Addendum. Report of the Fluid Dynamics Panel Working Group 04.

Experimental Data Base for Computers Program Assessment. Addendum. Report of the Fluid Dynamics Panel Working Group 04.
ADA147197

Publication Date	1984
Page Count	154
Abstract	Contents: Transonic Wing and Far Field Test Data on a High Aspect Ratio Transport Wing for Three Dimensional Computational Method Evaluation; Transonic Wing and Far Field Test Data on a Moderate Aspect Ratio Wing for Three Dimensional Computational Method Evaluation; Pressure Distributions Measured on Research Wing M100 Mounted on an Axisymmetric Body; Pressure Distribution Measured on Research Wing M86 Mounted on an Axisymmetric Body; and Pressure Distribution on a Swept Wing Aircraft in Flight.
Keywords	Aerodynamic configurations Aerodynamic characteristics Data bases Experimental data Swept wings Supercritical wings Aspect ratio Far field Pressure distribution Transonic characteristics Flight testing Wind tunnel models Two dimensional flow Three dimensional flow Supersonic flow Mathematical models Wing body configurations Great Britain Sweden United States Foreign technology NATO furnished
Source Agency	Non Paid ADAS
NTIS Subject Category	51A - Aerodynamics
Corporate Authors	Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine (France).
Supplemental Notes	Addendum to report dated May 79, AD-A073 982.
Document Type	Technical Report
Title Note	Advisory rept.
NTIS Issue Number	198503