WorldCat Identities

Schlichting, Hermann 1907-

Overview
Works: 142 works in 416 publications in 7 languages and 4,247 library holdings
Genres: Conference papers and proceedings 
Roles: Author, Honoree, Creator, Editor
Classifications: TL574.B6, 532.052
Publication Timeline
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Most widely held works by Hermann Schlichting
Boundary-layer theory by Hermann Schlichting( Book )

158 editions published between 1813 and 2006 in 7 languages and held by 2,621 WorldCat member libraries worldwide

Die berarbeitung fr die 10. deutschsprachige Auflage von Hermann Schlichtings Standardwerk wurde wiederum von Klaus Gersten geleitet, der schon die umfassende Neuformulierung der 9. Auflage vorgenommen hatte. Es wurden durchgngig Aktualisierungen vorgenommen, aber auch das Kapitel 15 von Herbert Oertel jr. neu bearbeitet. Das Buch gibt einen umfassenden berblick ber den Einsatz der Grenzschicht-Theorie in allen Bereichen der Strmungsmechanik. Dabei liegt der Schwerpunkt bei den Umstrmungen von Krpern (z.B. Flugzeugaerodynamik). Das Buch wird wieder den Studenten der Strmungsmechanik wie auch I
Aerodynamics of the airplane by Hermann Schlichting( Book )

33 editions published between 1959 and 2001 in 3 languages and held by 413 WorldCat member libraries worldwide

Ludwig Prandtl collected treatises on applied mechanics, hydro- and aerodynamics by W Tollmien( Book )

1 edition published in 1988 in English and held by 73 WorldCat member libraries worldwide

Ludwig Prandtl collected treatises on applied mechanics, hydro- and aerodynamics by W Tollmien( Book )

1 edition published in 1988 in English and held by 73 WorldCat member libraries worldwide

Aerodynamik des Tragflügels (Teil 2), des Rumpfes, der Flügel-Rumpf-Anordnung und der Leitwerke by Hermann Schlichting( Book )

5 editions published between 1960 and 2001 in German and held by 55 WorldCat member libraries worldwide

Grundlagen aus der Strömungsmechanik = Aerodynamik des Tragflügels (Teil 1) by Hermann Schlichting( Book )

4 editions published between 1959 and 1967 in German and held by 50 WorldCat member libraries worldwide

Bian jie ceng yuan li by Shi li xi ting( Book )

1 edition published in 2001 in Chinese and held by 36 WorldCat member libraries worldwide

Aerodynamik des Flugzeuges by Hermann Schlichting( Book )

4 editions published between 1960 and 1969 in German and held by 33 WorldCat member libraries worldwide

Grundlagen aus der Strömungstechnik, Aerodynamik des Tragflügels (Teil 1) by Hermann Schlichting( Book )

1 edition published in 2001 in German and held by 30 WorldCat member libraries worldwide

Hermann Schlichting--100 years : scientific colloquium celebrating the anniversary of his birthday, Braunschweig, Germany 2007 by Rolf Radespiel( Book )

2 editions published in 2009 in English and held by 21 WorldCat member libraries worldwide

This volume contains the contributions to the scientific anniversary colloquium in honor of the 100th birthday of Hermann Schlichting, Braunschweig, September2007. His outstanding achievements in boundary layer theory and aircraft aerodynamics are reviewed by invited scholars. Contributions of current leading research by the institutes formerly lead by Hermann Schlichting, the Institute of Fluid Mechanics of the Technische Universität Braunschweig and the Institute of Aerodynamics and Flow Technology of German Aerospace Center, in the fields of numerical flow simulation, experimental techniques, wing aerodynamics and turbomachinery highlight the lasting impact of his work until today
Berechnung der reibungslosen inkompressiblen Strömung für ein vorgegebenes ebenes Schaufelgitter by Hermann Schlichting( Book )

3 editions published in 1955 in German and held by 17 WorldCat member libraries worldwide

Aerodynamik des Flugzeuges by Hermann Schlichting( Book )

5 editions published between 1959 and 1967 in German and held by 17 WorldCat member libraries worldwide

Three-dimensional Boundary Layer Flow by Hermann Schlichting( Book )

6 editions published between 1961 and 1962 in German and English and held by 16 WorldCat member libraries worldwide

Discussion on aerodynamic aspects of V/STOL aeroplanes by Hermann Schlichting( Book )

5 editions published in 1961 in German and English and held by 11 WorldCat member libraries worldwide

Report on the special field "interference" to the wind tunnel committee in February 1945 by Hermann Schlichting( Book )

3 editions published in 1953 in English and held by 6 WorldCat member libraries worldwide

Contains an outline of investigations dealing with interference effects on the static stability of various airplane configurations that were conducted, were being conducted, and were started at the time of this report. Results of several investigations are presented and discussed briefly. A supplement is attached showing the configurations tested and outlining the various test programs. Suggestions for future investigations are also included
Laminar flow about a rotating body of revolution in an axial airstream by Hermann Schlichting( Book )

3 editions published in 1956 in English and held by 6 WorldCat member libraries worldwide

We have set ourselves the problem of calculating the laminar flow on a body of revolution in an axial flow which simultaneously rotates about its axis. The problem mentioned above, the flow about a rotating disk in a flow, which we solved some time ago, represents the first step in the calculation of the flow on the rotating body of revolution in a flow insofar as, in the case of a round nose, a small region about the front stagnation point of the body of revolution may be replaced by its tangential plane. In our problem regarding the rotating body of revolution in a flow, for laminar flow, one of the limiting cases is known: that of the body which is in an axial approach flow but does not rotate. The other limiting case, namely the flow in the neighborhood of a body which rotates but is not subjected to a flow is known only for the rotating circular cylinder, aside from the rotating disk. In the case of the cylinder one deals with a distribution of the circumferential velocity according to the law v = omega R(exp 2)/r where R signifies the cylinder radius, r the distance from the center, and omega the angular velocity of the rotation. The velocity distribution as it is produced here by the friction effect is therefore the same as in the neighborhood of a potential vortex. When we treat, in what follows, the general case of the rotating body of revolution in a flow according to the calculation methods of Prandtl's boundary-layer theory, we must keep in mind that this solution cannot contain the limiting case of the body of revolution which only rotates but is not subjected to a flow. However, this is no essential limitation since this case is not of particular importance for practical purposes
An approximate method for calculation of the laminar boundary layer with suction for bodies of arbitrary shape by Hermann Schlichting( Book )

3 editions published in 1949 in English and held by 5 WorldCat member libraries worldwide

Various ways were tried recently to decrease the friction drag of a body in a flow; they all employ influencing the boundary layer. One of them consists in keeping the boundary layer Laminar by suction; promising tests have been carried out. Since for large Reynolds numbers the friction drag of the laminar boundary layer is much lower than that of the turbulent boundary layer, a considerable saving in drag results from keeping the boundary layer laminar, even with the blower power required for suction taken into account. The boundary layer is kept laminar by suction in two ways: first, by reduction of the thickness of the boundary layer and second, by the fact that the suction changes the form of the velocity distribution so that it becomes more stable, in a manner similar to the change by a pressure drop. There by the critical Reynolds number of the boundary layer (USigma/V) (sub crit) becomes considerably higher than for the case without suction. This latter circumstance takes full effect only if continuous suction is applied which one might visualize realized through a porous wall. Thus the suction quantities required for keeping the boundary layer laminar become so small that the suction must be regarded as a very promising auxiliary means for drag reduction
Amplitude distribution and energy balance of small disturbances in plate flow by Hermann Schlichting( Book )

3 editions published in 1950 in English and held by 5 WorldCat member libraries worldwide

The distribution of the correlation coefficient and of the amplitude of the disturbance velocities is calculated as a function of the distance from the wall for two neutral disturbances, one at the lower and one at the upper branch of the neutral stability curve. The energy balance of the disturbance motion is also investigated and it is found that as required for neutral stability the energy of the disturbance motion that is dissipated by viscosity is equal to the energy transferred to the disturbance motion from the main flow during one cycle
Airfoil theory at supersonic speed by Hermann Schlichting( Book )

3 editions published in 1939 in English and held by 5 WorldCat member libraries worldwide

A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl airfoil theory of 1918-1919 for incompressible flow. In addition to the profile and induced drags, account must be taken at supersonic flow of still another drag, namely, the wave drag, which is independent of the wing aspect ratio. Both wave and induced drags are proportional to the square of the lift and depend on the Mach number, that is, the ratio of flight to sound speed. In general, in the case of supersonic flow, the drag-lift ratio is considerably less favorable than is the case for incompressible flow. Among others the following examples are considered: 1) lifting line with constant lift distribution (horseshoe vortex); 2) computation of wave and induced drag and the twist of a trapezoidal wing of constant lift density; 3) computation of the lift distribution and drag of an untwisted rectangular wing
Lecture series "boundary layer theory." by Hermann Schlichting( Book )

4 editions published in 1949 in English and held by 3 WorldCat member libraries worldwide

The subject of turbulent flow is treated in detail. The available data on flow through pipes and over flat plates are presented. Turbulent wakes and jets are treated by means of the Prandtl mixing length theory. A section is devoted to the Gruschwitz method for calculating turbulent boundary layers in accelerated and retarded flows. The methods of Betz and Jones for determining profile drag from wake surveys are given. A chapter on the theory of the stability of the laminar boundary layer, developed from the point of view of small oscillations, is also included
 
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Boundary-layer theory
Alternative Names
Hermann Schlichting German engineer

Hermann Schlichting tysk ingenir

Hermann Schlichting tysk ingenjr

Schlichting, H.

Schlichting, H. 1907-

Schlichting, H. 1907-1982

Schlichting, H. (Hermann), 1907-

Schlichting, Hermann

Schlichting Herrmann

Schlichting, Herrmann 1907-

Schlichting, Herrmann 1907-1982

Šlihting, G.

Шлихтинг, Герман

Languages
Covers
Aerodynamics of the airplaneAerodynamik des Tragflügels (Teil 2), des Rumpfes, der Flügel-Rumpf-Anordnung und der LeitwerkeGrundlagen aus der Strömungstechnik, Aerodynamik des Tragflügels (Teil 1)Hermann Schlichting--100 years : scientific colloquium celebrating the anniversary of his birthday, Braunschweig, Germany 2007