Cover Image

The design of supercritical wings by the use of three-dimensional transonic theory/

Main Author:	Mann, Michael J.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979
Series:	NASA technical paper 1400
Subjects:	Airplanes > Wings, Swept-back > Design and construction Airplanes, Military

Similar Items

Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds/
by: Henderson, William P.
Published: (1976)

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration/
by: Coe, Paul L., Jr.
Published: (1979)

Effects of wing leading-edge deflection on low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration/
by: Coe, Paul L., Jr.
Published: (1979)

Aerodynamic derivatives for an oblique wing aircraft estimated from flight data by using a maximum likelihood technique/
by: Maine, Richard E.
Published: (1978)

Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings/
by: Carlson, Harry W.
Published: (1988)

Nonlinear wave interactions in swept wing flows/
by: El-Hady, Nabil M.
Published: (1988)

A swept wing panel in a low speed flexible walled test section/
by: Goodyer, M. J.
Published: (1987)

Dual methods and approximation concepts in structural synthesis/
by: Fleury, Claude
Published: (1980)

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing/
by: Coe, Paul L., Jr.
Published: (1983)

Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing/
by: Darden, Christine M.
Published: (1989)

German development of the swept wing 1935-1945 /
Published: (2010)

Leading-edge deflection optimization for a highly swept arrow-wing configuration/
by: Coe, Paul L., Jr.
Published: (1980)

Strain-gage bridge calibration and flight loads measurements on a low-aspect-ratio thin wing/
by: Peele, Ellwood L.
Published: (1975)

Design and fabrication of composite wing panels containing a production splice/
by: Reed, D. L.
Published: (1975)

Subsonic panel method for designing wing surfaces from pressure distribution/
by: Bristow, D. R.
Published: (1983)

A transonic-small-disturbance wing design methodology/
by: Phillips, Pamela S.
Published: (1988)

Analytical study of a free-wing/free-trimmer concept/
Published: (1978)

Downstream influence of swept slot injection in hypersonic turbulent flow/
by: Hefner, Jerry N.
Published: (1977)

Flight measurements of surface pressures on a flexible supercritical research wing/
by: Eckstrom, Clinton V.
Published: (1985)

A method for the design of transonic flexible wings/
by: Smith, Leigh Ann
Published: (1990)

Wing theory/
by: Jones, Robert T. 1910-
Published: (1990)

Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls/
by: Luckring, James M.
Published: (1978)

Application of a structural optimization procedure for advanced wings
by: Godel, H.
Published: (1981)

Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction/
by: Dagenhart, J. Ray
Published: (1981)

Recent transonic flutter investigations for wings and external stores
Published: (1983)

Aeroelastic loads prediction for an arrow wing/
Published: (1983)

Wing theory /
by: Jones, Robert T. 1910-1999,

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5/
by: Mack, Robert J.
Published: (1988)

Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds/
by: Stallings, Robert L.
Published: (1980)

Performance evaluation method for dissimilar aircraft designs/
by: Walker, Harold J.
Published: (1979)

Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62/
Published: (1981)

Theoretical parametric study of the relative advantages of winglets and wing-tip extensions/
by: Heyson, Harry H.
Published: (1977)

Wind-tunnel investigation of a variable camber and twist wing/
by: Ferris, James C.
Published: (1977)

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds/
by: Stallings, Robert L.
Published: (1981)

Assessment of wingtip modifications to increase the fuel efficiency of Air Force aircraft
Published: (2007)

Effects of winglets on a first-generation jet transport wing : VII, sideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model /
by: Meyer, Robert R.
Published: (1986)

A study of canard-wing interference using experimental pressure data at transonic speeds/
by: Gloss, Blair B.
Published: (1979)

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles/
by: Sleeman, William C.
Published: (1975)

Effect of winglets on a first-generation jet transport wing : III pressure and spanwise load distributions for a semispan model at Mach 0.30 /
by: Montoya, Lawrence C.
Published: (1977)

Effect of winglets on a first-generation jet transport wing : II pressure and spanwise load distributions for a semispan model at high subsonic speeds /
by: Montoya, Lawrence C.
Published: (1977)

Cannot write session to /tmp/vufind_sessions/sess_tnm7bv44dmutpjm73amnsfduj3