Add to ORKGThis status paper reviews the experimental ground test program of the High Alpha Technology Program (HATP). The reasons for conducting this ground test program had their origins during the 1970's when several difficulties were experienced during the development programs of both the F-18 and F-16. A careful assessment of ground test to flight correlations appeared to be important for reestablishing a high degree of confidence in our ground test methodology. The current paper will then focus on one aspect of the HATP program that is intended to improve the correlation between ground test and flight, high-alpha gritting. The importance of this work arises from the sensitivity of configurations with smooth-sided forebodies to Reynolds number. A...
High-angle-of-attack aerodynamic studies have been conducted on both the F18 High Alpha Research Veh...
A review is presented in viewgraph format of an ongoing NASA/U.S. Navy study to determine control po...
As future aircraft migrate toward tailless, blended wing body configurations, aircraft designers are...
Determining the baseline aerodynamics of the F/A-18 was one of the major objectives of the High-Angl...
A subsonic study of high-angle-of-attack gritting strategies was undertaken with a 0.06-scale model ...
Determining the baseline aerodynamics of the F/A-18 was one of the major objectives of the High-Angl...
The F-18 High Alpha Research Vehicle has proven to be a useful research tool with many unique capabi...
This paper gives an overview of the NASA F-18 High Alpha Research Vehicle. The three flight phases o...
Pressure distributions measured on the forebody and the leading-edge extensions (LEX's) of the NASA ...
The goal of the Fourth High Alpha Conference was to focus on the flight validation of high angle-of-...
The NASA F/A-18 High Alpha Research Vehicle (HARV) has been the flight test bed of a focused technol...
Pressure distributions were obtained at nearly identical fuselage stations and wing chord butt lines...
A major goal of the NASA High-Angle-of-Attack Technology Program (HATP) has been to help develop tec...
The methods by which aerodynamic coefficients are determined and discussed. These include: calculati...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
High-angle-of-attack aerodynamic studies have been conducted on both the F18 High Alpha Research Veh...
A review is presented in viewgraph format of an ongoing NASA/U.S. Navy study to determine control po...
As future aircraft migrate toward tailless, blended wing body configurations, aircraft designers are...
Determining the baseline aerodynamics of the F/A-18 was one of the major objectives of the High-Angl...
A subsonic study of high-angle-of-attack gritting strategies was undertaken with a 0.06-scale model ...
Determining the baseline aerodynamics of the F/A-18 was one of the major objectives of the High-Angl...
The F-18 High Alpha Research Vehicle has proven to be a useful research tool with many unique capabi...
This paper gives an overview of the NASA F-18 High Alpha Research Vehicle. The three flight phases o...
Pressure distributions measured on the forebody and the leading-edge extensions (LEX's) of the NASA ...
The goal of the Fourth High Alpha Conference was to focus on the flight validation of high angle-of-...
The NASA F/A-18 High Alpha Research Vehicle (HARV) has been the flight test bed of a focused technol...
Pressure distributions were obtained at nearly identical fuselage stations and wing chord butt lines...
A major goal of the NASA High-Angle-of-Attack Technology Program (HATP) has been to help develop tec...
The methods by which aerodynamic coefficients are determined and discussed. These include: calculati...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
High-angle-of-attack aerodynamic studies have been conducted on both the F18 High Alpha Research Veh...
A review is presented in viewgraph format of an ongoing NASA/U.S. Navy study to determine control po...
As future aircraft migrate toward tailless, blended wing body configurations, aircraft designers are...