1-15 of 15 Books
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
By Richard J. Re
Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
By Elizabeth B. Plentovich
Rocket-based combined cycle engine technology development
Rocket-based combined cycle engine technology development
By J. R. DeBonis
Study of CFD methods applied to rapidly deforming boundaries
Study of CFD methods applied to rapidly deforming boundaries
By John W. Slater
PSP measurement of stator vane surface pressures in a high speed fan
PSP measurement of stator vane surface pressures in a high speed fan
By Jan Lepicovsky
Analysis of fluctuating static pressure measurements in the National Transonic Facility
Analysis of fluctuating static pressure measurements in the National Transonic Facility
By William B. Igoe
Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
By E. Allen Arrington
Method for determining the time delay of the pitot-static tubing system of aircraft
Method for determining the time delay of the pitot-static tubing system of aircraft
By J. H. Breeman
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
By Richard J. Re
The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
By Elizabeth B. Plentovich
Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
By D. M. Schuster
Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
By Williams, J. G.
Static presssure position error calibration of the NAE T-33 C-FSKH
Static presssure position error calibration of the NAE T-33 C-FSKH
By J. F. Aitken
A preliminary look at techniques used to obtain airdata from flight at high angles of attack
A preliminary look at techniques used to obtain airdata from flight at high angles of attack
By Timothy R. Moes
Experimental cavity pressure measurements at subsonic and transonic speeds
Experimental cavity pressure measurements at subsonic and transonic speeds
By Elizabeth B. Plentovich