Cover Image

Wing theory in supersonic flow /

Show other versions (1)

Bibliographic Details
Main Author:	Carafoli, Elie
Other Authors:	Mateescu, Dan, Năstase, Adriana
Format:	Book
Language:	English
Published:	Oxford, New York : Pergamon Press, [1969]
Edition:	[1st. ed.].
Series:	International series of monographs in aeronautics and astronautics. Division II: Aerodynamics, v. 7
Subjects:	Aerodynamics, Supersonic. Airplanes > Wings.

Similar Items

Wing theory in supersonic flow /
by: Carafoli, Elie, et al.
Published: (1969)

The theory of thin wings in subsonic flow /
by: Belot︠s︡erkovskiĭ, S. M. (Sergeĭ Mikhaĭlovich)
Published: (1967)

Selected works on wing theory /
by: Chaplygin, Sergeĭ Alekseevich, 1869-1942
Published: (1956)

Theory of wing sections : including a summary of airfoil data /
by: Abbott, Ira Herbert, 1906-
Published: (1959)

Theory of wing sections : including a summary of airfoil data /
by: Abbott, Ira Herbert, 1906-
Published: (1949)

The theory of thin wings in subsonic flow /
by: Belot︠s︡erkovskiĭ, S. M. (Sergeĭ Mikhaĭlovich)
Published: (1967)

A new method for calculating the two-dimensional subsonic flow on thin wing profiles with small angles of incidence = Neuere Methode zur Berechung der ebenen Unterschallstromung an dunnen Profilen bei kleinen Anstellwinkeln /
by: Gretler, W.
Published: (1968)

Calculation method for the reaction of a gust of wind on a thin wing of arbitrary planform = Metod rascheta vozdeistviyar por'iva na proizvol'noe tonkoe krilo /
by: Belot︠s︡erkovskiĭ, S. M. (Sergeĭ Mikhaĭlovich)
Published: (1968)

Half-body and wing combinations in supersonic flow : a review of some principles and possibilities /
by: Goldsmith, E. L.
Published: (1968)

Measurement of the pitching-moment derivatives for rigid tapered wings of hexagonal planform oscillating in supersonic flow /
by: Woodgate, L.
Published: (1962)

A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow /
by: Eldridge, Robert Henry
Published: (1968)

Wind tunnel test of composite wing extensions : test number 8112 & 8115 /
by: Nicks, Oran W.
Published: (1982)

Wind tunnel test of a composite wing extension designed for a specific application : test number 8203 /
by: Nicks, Oran W.
Published: (1982)

Theory of wing sections : including a summary of airfoil data /
by: Abbott, Ira H.
Published: (1999)

An experimental investigation at supersonic speeds of the characteristics of two gothic wings, one plane and one cambered /
by: Squire, Leonard Charles
Published: (1961)

The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow /
by: Smith, Jeremy H. B.
Published: (1967)

The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight /
by: Davies, Danny E.
Published: (1962)

The vortex of appendage-body junction flow control using suitable fillets /
by: Li, Ding
Published: (1995)

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

Tonkai︠a︡ nesushchai︠a︡ poverkhnostʹ v dozvukovom potoke gaza /
by: Belot︠s︡erkovskiĭ, S. M. (Sergeĭ Mikhaĭlovich)
Published: (1965)

Some exact calculations of the lift and drag produced by a wedge in supersonic flow : either directly or by interference /
by: Roe, P. L.
Published: (1967)

Some calculations of the take-off behaviour of a slender-wing supersonic transport design constrained to follow a specified pitch-attitude time history /
by: Tomlinson, Barry Nigel
Published: (1967)

Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds /
by: Roper, G. M.
Published: (1961)

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls /
by: Isaacs, Donald
Published: (1969)

Morphing wing technologies : large commercial aircraft and civil helicopters /
Published: (2018)

Pressure-plotting and force tests at Mach numbers up to 2.8 on an uncambered slender wing of p = 1/2, s/co = 1/4 ('Handley Page Ogee') /
by: Courtney, Adrian Laurence
Published: (1964)

Experiments at M b0 s= 4.03 on two families of pressure-plotting wing-and-half-cone combinations /
by: Rogers, E. W. E.
Published: (1967)

Morphing wing technologies : large commercial aircraft and civil helicopters /
Published: (2018)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory /
by: Harris, G. Z.
Published: (1967)

Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
by: Blair, A. B.
Published: (1976)

The potential theory of unsteady supersonic flow.
by: Miles, John Wilder
Published: (1959)

A theory of supercritical wing sections : with computer programs and examples /
by: Bauer, Frances
Published: (1972)

Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)

Some mutual interference effects between a 5.7 cone and sonic-leading-edge delta wing at M..-2.49 /
by: Goldsmith, E. L.
Published: (1967)

Supercritical wing sections II : a handbook /
Published: (1975)

Engineering supersonic aerodynamics.
by: Bonney, E. Arthur
Published: (1950)

Linearized theory of supersonic flow /
by: Goldstein, Sydney, 1903-1989
Published: (1950)

Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /
by: Wood, Richard M., et al.
Published: (1985)

Pressure distribution on two wings with curved leading edges at supersonic speeds /
by: Narayan, K. Yegna
Published: (1974)