Effect of sweep on cavity flow fields at subsonic and transonic speeds /

Flight tests of a supersonic natural laminar flow airfoil /
by: Frederick, Michael A.
Published: (2015)

Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications /
by: Hahne, David E. (David Edgar)
Published: (1999)

Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 /
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)

Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /
by: Erickson, Gary E.
Published: (2013)

An unsteady time asymptotic flow in the square driven cavity /
by: Goodrich, John W., 1945-
Published: (1990)

Multigrid approach to incompressible viscous cavity flows /
by: Wood, W. A.
Published: (1996)

Trailing edge flow conditions as a factor in airfoil design /
by: Ormsbee, A. I.
Published: (1984)

F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data /
by: Fisher, David F.
Published: (1990)

Prediction of sound fields in acoustical cavities using the boundary element method /
by: Kipp, Carl R.
Published: (1985)

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /
by: Hallissy, James B.
Published: (1989)

Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /
by: Erickson, Gary E.
Published: (2013)

Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 /
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 /
by: Re, Richard J., et al.
Published: (1996)

Pressure-distribution measurements on a transonic low-aspect ratio wing /
by: Keener, Earl R.
Published: (1985)

Large-scale advanced propeller blade pressure distributions : predictions and data /
Published: (1989)

Three-dimensional flow field measurements in a transonic turbine cascade /
by: Giel, P. W.
Published: (1996)

Advanced noise control fan aerodynamic performance /
by: Bozak, Richard F., Jr
Published: (2009)

Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /
by: Campbell, Bryan A.
Published: (1999)

Compressor study to meet large civil tilt rotor engine requirements /
by: Veres, Joseph P.
Published: (2009)

Heat transfer in a complex trailing edge passage for a high pressure turbine blade.
by: Rigby, D. L. (David Lester), 1963-
Published: (2002)

Thrust measurement of Dielectric Barrier Discharge (DBD) plasma actuators : new anti-thrust hypothesis, frequency sweeps methodology, humidity and enclosure effects /
by: Ashpis, D. E. (David E.), et al.
Published: (2014)

Aero-heating of shallow cavities in hypersonic freestream flow /
Published: (2010)

An experimental study of the turbulent boundary layer on a transport wing in subsonic and transonic flow /
by: Spaid, Frank W.
Published: (1990)

Jet surface interaction, scrubbing noise /
by: Khavaran, Abbas, 1953-
Published: (2013)

Experimental effects of wing location on wing-body pressures at supersonic speeds /
by: Allen, Jerry M., et al.
Published: (1993)

An airfoil flutter model suspension system to accommodate large static transonic airloads /
by: Reed, Wilmer H.
Published: (1985)

Predicting modes of the unsteady vorticity field near the trailing edge of a blade /
by: Devenport, William J.
Published: (2003)

Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows : progress report for the period ended December 31, 1989 /
by: Singh, D. J.
Published: (1990)

Design of a slotted, natural-laminar-flow airfoil for a transport aircraft /
by: Somers, Dan M.
Published: (2019)

Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system /
by: Maddalon, Dal V., et al.
Published: (1990)

Flight test results from the rake airflow gage experiment on the F-15B airplane /
by: Frederick, Michael A.
Published: (2011)

Experimental study of bubble cavities attached to a rotating shaft in a reservoir /
by: Hendricks, Robert C.
Published: (1984)

Pressure probe designs for dynamic pressure measurements in a supersonic flow field /
by: Porro, A. Robert
Published: (2001)

Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a crosswind /
Published: (1985)

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber /
by: McMillin, S. Naomi (Susan Naomi)
Published: (1996)

Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility /
by: Bozak, Richard F.
Published: (2018)