Cover Image

Wing leading edge joint laminar flow tests /

Bibliographic Details
Main Author:	Drake, Aaron (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, October 1996.
Series:	NASA technical memorandum ; 4762.
Subjects:	F-104 aircraft. Laminar flow airfoils. Friction measurement. Skin friction. Pressure distribution.
Online Access:	https://purl.fdlp.gov/GPO/gpo65484

Similar Items

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

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)

An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique /
by: Hwang, Danny P.
Published: (1999)

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

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

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)

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

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)

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

Laminar flow aircraft certification /
by: Williams, Louis J.
Published: (1986)

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

A proof of concept experiment for reducing skin friction by using a micro-blowing technique /
by: Hwang, Danny P.
Published: (1996)

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

Effectiveness of micro-blowing technique in adverse pressure gradients /
by: Welch, Gerard E.
Published: (2001)

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

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

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

Enhanced viscous flow drag reduction using acoustic excitation : final report /
by: Nagel, R. T.
Published: (1988)

Enhanced viscous flow drag reduction using acoustic excitation : final report /
by: Nagel, R. T.
Published: (1988)

Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel /
by: Watkins, A. Neal
Published: (2015)

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

Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet /
by: Maglieri, Domenic J.
Published: (2011)

Aerodynamic design of a propeller for high-altitude balloon trajectory control /
by: Eppler, Richard, et al.
Published: (2012)

Measurement of gear tooth dynamic friction /
by: Rebbechi, Brian, et al.
Published: (1996)

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

Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
by: Powell, A. G.
Published: (1989)

Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
by: Powell, A. G.
Published: (1989)

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade /
by: Buffum, Daniel H.
Published: (1996)

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

NASA Boeing 737 aircraft test results from 1996 joint winter runway friction measurement program /
by: Yager, Thomas
Published: (1996)

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

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)

Natural laminar flow flight experiments on a swept wing business jet- boundary layer stability analyses /
by: Rozendaal, R. A.
Published: (1986)

Visualization of flows in packed beds of twisted tapes /
by: Hendricks, Robert C.
Published: (2002)

Visualization of flows in packed beds of twisted tapes /
Published: (2002)

The MillSOT--a spiral orbit tribometer on a milling machine /
by: Pepper, Stephen V., 1937-
Published: (2014)

Durability evaluation of selected solid lubricating films /
by: Miyoshi, Kazuhisa
Published: (2001)

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

Aerodynamic classification of swept-wing ice accretion /
by: Diebold, Jeff M., et al.
Published: (2013)