Flight tests of a supersonic natural laminar flow airfoil /

Flight demonstration of a shock location sensor using constant voltage hot-film anemometry /
by: Moes, Timothy R., et al.
Published: (1997)

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)

An approach to the constrained design of natural laminar flow airfoils /
by: Green, Bradford E.
Published: (1997)

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis /
by: Brooks, Cuyler W., Jr
Published: (1991)

Delay of transition using forced damping /
by: Exton, Reginald J.
Published: (2014)

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)

An exploratory investigation of a slotted, natural-laminar-flow airfoil /
by: Somers, Dan M.
Published: (2012)

Design of a slotted, natural-laminar-flow airfoil for business-jet applications /
by: Somers, Dan M.
Published: (2012)

Effect of sweep on cavity flow fields at subsonic and transonic speeds /
Published: (2012)

Structural tests and development of a laminar flow control wing surface composite chordwise joint /
by: Lineberger, L. B.
Published: (1984)

Potential flow analysis of glaze ice accretions on an airfoil /
by: Zaguli, Ronald J.
Published: (1984)

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)

Laminar flow aircraft certification : proceedings of a workshop : sponsored by the National Aeronautics and Space Administration, the American Institute of Aeronautics and Astronautics, the Society of Automotive Engineers, and the Federal Aviation Administration, and held at Wichita, Kansas, April 15-16, 1985 /
Published: (1986)

Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil /
by: Hahne, David E. (David Edgar)
Published: (1991)

Design of fuselage shapes for natural laminar flow /
by: Dodbele, S. S., et al.
Published: (1986)

Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows /
Published: (1991)

Experimental observations on the deformation and breakup of water droplets near the leading edge of an airfoil /
by: Vargas Meza, Mario
Published: (2011)

Calibration of sonic valves for the laminar flow control, leading-edge flight test /
by: Petley, D. H.
Published: (1985)

Flow visualization by elastic light scattering in the boundary layer of a supersonic flow /
by: Herring, Gregory C.
Published: (2000)

Mechanism of water droplet breakup near the leading edge of an airfoil /
by: Vargas, Mario, et al.
Published: (2012)

An asymptotic analysis of supersonic reacting mixing layers /
by: Jackson, T. L.
Published: (1987)

Computer program to obtain ordinates for NACA airfoils /
by: Ladson, Charles L.
Published: (1996)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

Wing leading edge joint laminar flow tests /
by: Drake, Aaron
Published: (1996)

Modelling the transitional boundary layer /
by: Narasimha, R.
Published: (1990)

Subsonic ultra green aircraft research phase II-volume I-3 /
by: Bradley, Marty K., et al.
Published: (2014)

The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity /
by: Duck, Peter W.
Published: (1991)

Aerodynamic characterization of a thin, high-performance airfoil for use in ground fluids testing /
by: Broeren, Andy P., et al.
Published: (2013)

Inverse boundary-layer theory and comparison with experiment /
by: Carter, James E. (James Edward), 1944-
Published: (1978)

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

Artificial boundary conditions for computation of oscillating external flows /
by: Tsynkov, S. V.
Published: (1996)

Boundary layer stability and transition to turbulence : presented at the First ASME JSME Fluids Engineering Conference, Portland, Oregon, June 23-27, 1991 /
Published: (1991)

Optimization of an advanced design three-element airfoil at high Reynolds numbers /
by: Lin, J.-C. (Jiun-Chuan), et al.
Published: (1995)

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)

The use of hot-film technique for boundary layer studies on a 21% thick airfoil = Utilisation de la technique du film chaud pour des études de couche limite autour d'un profil d'aile d'une épaisseur relative de 21% /
by: Khalid, M.
Published: (1987)

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /
by: Applin, Zachary T.
Published: (1990)