Hostname: page-component-586b7cd67f-g8jcs Total loading time: 0 Render date: 2024-11-28T17:10:24.909Z Has data issue: false hasContentIssue false
  • English
  • Français

Aeronautical Research in the Netherlands

Published online by Cambridge University Press:  28 July 2016

H. J. Van Der Maas
Get access Rights & Permissions [Opens in a new window]

Extract

It is a great honour to be invited to present a survey of the aeronautical research in the Netherlands to this distinguished audience and I wish to express my thanks to the Council of the Royal Aeronautical Society for giving me the opportunity to deliver this lecture. The more I appreciate it in view of the friendship between our two countries, between the Society and its Dutch counterpart and the personal friendship with so many present on this occasion.

It is my intention to give a survey of some of the work performed in the Netherlands in the post-war period and to describe briefly the main installations which are now available or under construction. I hope that I will be able to give you an impression of the scope and the nature of the aeronautical research activities in the Netherlands. These activities are being directed in the first place by the immediate needs of the industry and the aircraft operators; and in the second place by the desire to contribute to the general development of the art, thereby also supporting the exchange of results on an international basis, even more essential than before, considering the rapidly growing importance of aviation in its broadest sense.

Before entering into more technical matters it may be worthwhile to give very briefly an outline of the present organisation of aeronautical research and development in the Netherlands.

Type
Research Article
Information
The Aeronautical Journal , Volume 61 , Issue 557 , May 1957 , pp. 295 - 334
Copyright
Copyright © Royal Aeronautical Society 1957

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Refenences

1. Landstra, J. A. (1955). A study of some factors affecting the stability, contributed by a horizontal tail at various vertical positions behind a swept-back wing, especially at high angles of attack. N.L.L. Report A. 1385, 1955 (in Dutch).Google Scholar
2. Neut, A. Van Der (1953). Some problems occurring in structural design and analysis of welded variable density wind tunnels. Communication presented at the Third General AGARD Assembly, London, 3rd-llth September 1953.Google Scholar
3. Erdmann, S. F. (1951). Technische Möglichkeiten des 3 x 3 cm2 Ueberschallkanals des N.L.L. und beabsichtigte Untersuchungen. N.L.L. Report F.84, 1951.Google Scholar
4. Erdmann, S. F. and Meyer, A. W. (1951). Investigations of diffusers for the projected 40 X 40 cm2 supersonic wind tunnel of the N.L.L. N.L.L. Report F. 80, 1951 (in Dutch).Google Scholar
5. Spijkers, A. A. and Meyer, A. W. (1951). Investigations at M = 6in the 3 x 3 cm2 supersonic wind tunnel of the N.L.L. N.L.L. Report F. 98, 1951 (in Dutch).Google Scholar
6. Erdmann, S. F. (1951). Ein neues, sehr einfaches Interferometer zum Erhalt quantitativ auswertbarer Strömungsbilder. Applied Scientific Research, Vol. B2, Doctor Thesis, Aachen, 1951.Google Scholar
7. Erdmann, S. F. (1946). Numerische Behandlung der Charakteristieken Methode beim Entwurf von Ueberschallduüsen. N.L.L. Report F. 2, 1946.Google Scholar
8. Erdmann, S. F. (1947). Entwurf von Ueberschallduüsen mit zeichnerischen Diskussion des Anfangswertproblems. N.L.L. Report F. 5, 1947.Google Scholar
9. Erdmann, S. F. (1947). Note on the problem of initial values in the design of supersonic nozzles in connection with measured velocity distribution. N.L.L. Report F. 21, 1947.Google Scholar
10. Baumhauer, H. G. Von and Koning, C. (1922). On the stability of oscillation of a wing-flap system. N.L.L. Report A 48, 1922 (in Dutch).Google Scholar
11. Vooren, A. I. Van de and Greidanus, J. H. (1945). Diagrams of critical flutter speed for wings of a certain standard type. N.L.L. Report V. 1297, 1945.Google Scholar
12. Vooren, A. I. Van de (1947). The change in nutter speed due to small variations in some aileron parameters. N.L.L. Report V. 1380, 1947.Google Scholar
13. Vooren, A. I. Van de (1947). Diagrams of flutter, divergence and aileron reversal speeds for wings of a certain standard type. N.L.L. Report V. 1397, 1947.Google Scholar
14. Vooren, A. I. Van de (1952). Theory and practice of flutter calculations for systems with many degrees of freedom. N.L.L. Report F. 100, 1952, Doctor Thesis, Delft.Google Scholar
15. Küssner, H. G. (1935). Augenblicklicher Entwicklungsstand der Frage des Flugelflatterns. Luftfahrtforschung, Band 12, p. 193, 1935.Google Scholar
16. Theodorsen, TH. (1940). General theory of aerodynamic instability and the mechanism of flutter. N.A.C.A. Report 496, 1940.Google Scholar
17. Greidanus, J. H., Vooren, A. I. Van de and Bergh, H. (1952). Experimental determination of aerodynamic coefficients of an oscillating wing in incompressible, twodimensional flow. Part I. Experiments with fixed axis of rotation. N.L.L. Report F. 101, 1952.Google Scholar
18. Vooren, A. I. Van de and Bergh, H. (1952). Experimental determination of aerodynamic coefficients of an oscillating wing in incompressible, two-dimensional flow. Part II. Experiments with moving axis of rotation. N.L.L. Report F. 102, 1952.Google Scholar
19. Bergh, H. (1952). Experimental determination of aerodynamic coefficients of an oscillating wing in incompressible, two-dimensional flow. Part III. Experiments at zero airspeed. N.L.L. Report F. 103, 1952.Google Scholar
20. Bergh, H. and Vooren, A. I. Van de(1952). Experimental determination of the aerodynamic coefficients of an oscillating wing in incompressible, two-dimensional flow. Part IV. Calculation of the coefficients. N.L.L. Report F. 104, 1952.Google Scholar
21. Bergh, H. (1956). Experimental determination of the aerodynamic forces on an oscillating wing with control surfaces in incompressible, two-dimensional flow. N.L.L. Report F. 175, 1956.Google Scholar
22. Timman, R. (1946). Considerations on the aerodynamic forces on oscillating aerofoils in compressible flow. Doctor Thesis, Delft, 1946 (in Dutch).Google Scholar
23. Timman, R. and Vooren, A. I. Van de(1949). Theory of the oscillating wing with aerodynamically balanced control surface in a two-dimensional flow. N.L.L. Report F. 54, 1949.Google Scholar
24. Timman, R., Vooren, A. I. Van de and Greidanus, I. H. (1954). Aerodynamic coefficients of an oscillating airfoil in two-dimensional subsonic flow. Journal of the Aeronautical Sciences, Vol. 21, p. 499, July 1954.Google Scholar
25.Tables of aerodynamic coefficients for an oscillating wing-flap system in a subsonic compressible flow. N.L.L. Report F. 151, 1954.Google Scholar
26. Jager, E. M. De (1954). Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic compressible flow. N.L.L. Report F. 155, 1954.Google Scholar
27. Ijff, J. (1952). Influence of compressibility on the calculated flexure-torsion flutter speed of a family of rectangular cantilever wings. N.L.L. Report F. 118, 1952.Google Scholar
28. Ijff, J., Bosschaart, A. C. A. and Vooren, A. I. Van de (1954). Influence of compressibility on the flutter speed of a family of rectangular cantilever wings with aileron. N.L.L. Report F. 147, 1954.Google Scholar
29. Reissner, E. (1947). Effect of finite span on the airload distribution for oscillating wings. N.A.C.A. T.N. 1194, 1195, 1947.Google Scholar
30. Jones, W. P. (1952). The calculation of aerodynamic derivative coefficients for wings of any plan form in nonuniform flow. A.R.C., R. and M. 2470, 1952.Google Scholar
31. Spiegel, E. Van, and Timman, R. (1956). Linearized aerodynamic theory for wings of circular planform in steady and unsteady incompressible flow. N.L.L. Report M.P. 134, 1956.Google Scholar
32. Timman, R. (1950). The aerodynamic forces on oscillating propeller blades. N.L.L. Report F. 69, 1950.Google Scholar
33. Greidanus, J. H., Timman, R. and Zaat, J. A. (1952). The Aerodynamic Forces on Oscillating Blades of a Helicopter Rotor with Finite Span, Rotating in Still Air. N.L.L. Report F. 108, 1952.Google Scholar
34. Timman, R. (1956). The Aerodynamic Forces on Oscillating Helicopter Blades. N.L.L. Report F. 181, 1956.Google Scholar
35. Vooren, A. I. Van de (1952). Flutter of a Helicopter Rotor Without Forward Speed. N.L.L. Report F. 109, 1952.Google Scholar
36. Meijer drees, J., Lucassen, L. R. and Hendal, W. P. (1949). Airflow Through Helicopter Rotors in Vertical Flight. N.L.L. Report V. 1535, 1949.Google Scholar
37. Aarssen, R. J. (1956). Flow Field Measurements Near the Tip of a Model Helicopter Rotor with Non-Operating Ramjets. N.L.L. Report H-4, 1956 (in Dutch).Google Scholar
38. Zaat, J. A., Spiegel, E. Van, and Timman, R. (1955). The Three-Dimensional Laminar Boundary Layer Flow About a Yawed Ellipsoid at Zero Incidence. N.L.L. Report F. 165, 1955.Google Scholar
39. Zaat, J. A. (1956). A Simplified Method for the Calculation of Three-Dimensional Laminar Boundary Layers. N.L.L. Report F 184, 1956.Google Scholar
40. Timman, R., Zaat, J. A., and Burgerhout, TH. J. (1956). Stability Diagrams for Laminar Boundary Layer Flow. N.L.L. Report F. 193, 1956.Google Scholar
41. Schubauer, G. B. and Skramstad, H. K. (1948). Laminar Boundary Layer Oscillations and Transition on a Flat Plate. N.A.C.A. T.R. 909, 1948.Google Scholar
42. Tollmien, W. (1929). Ueber die Entstehung der Turbulenz. Nach. Ges. Wiss. Göttingen. Math. Phys. Klasse 21, 1929.Google Scholar
43. Lin, C. C. (1945, 1946). On the Stability of Two- Dimensional Parallel Flows. Quarterly of Applied Mathematics. Vol. 3, pp. 117–142, 218-234, 277-301, 1945, 1946.Google Scholar
44. Schlichting, H. (1933). Zur Entstehung der Turbulenz bei der Plattenströmung. Nachr. Ges. Wiss. Göttingen. Math. Phys. Klasse 182, 1933.Google Scholar
45. Greidanus, J. H. (1948). The Loading of Aeroplane Structures by Symmetrical Gusts. N.L.L. Reports and Transactions. Vol. XIV, 1948 (in Dutch).Google Scholar
46. Greidanus, J. H. and Vooren, A. I. Van de(1948). Gust Load Coefficients for Wing and Tail Surfaces of an Aeroplane. N.L.L. Report F. 28, 1948.Google Scholar
47. Vooren, A. I. Van de (1948). Loads on Wing and Tail Surfaces of an Aeroplane Due to a Sinusoidal Gust Wave. N.L.L. Report F. 33, 1948.Google Scholar
48. Greidanus, J. H. and Vooren, A. I. Van de(1949). Proposal for an airworthiness requirement referring to symmetrical gust loads. N.L.L. Report F. 45, 1949.Google Scholar
49. Vooren, A. I. Van de, and Ijff, J. (1953). Investigation of the Effect of a System of Automatic Gust Load Alleviation on the Critical Flutter Speed of the Fokker F.27. N.L.L. Report F.126, 1953 (In Dutch).Google Scholar
50. Vooren, A. I. Van de and Jager, E. M. DE (1956). Calculation of Aerodynamic Forces on Slowly Oscillating Rectangular Wings in Subsonic Flow. N.L.L. Report F. 192, 1956.Google Scholar
51. Marx, A. J. and Buhrman, J. (1946). General Considerations on the Flight Characteristics of Tailless Aircraft. N.L.L. Report V. 1399, V. 1400 and V. 1401, 1946 (in Dutch).Google Scholar
52. Marx, A. J. and Buhrman, J. (1949). The Effect of a Spring Tab Elevator on the Static Longitudinal Stability of an Aeroplane. N.L.L. Report V. 1547, Reports and Transactions, Vol. XV, 1949.Google Scholar
53. Marx, A. J. and Buhrman, J. (1952). Analysis of the Pitching Motion of an Aeroplane Due to Sideslip. N.L.L. Report V. 1602, Reports and Transactions. Vol. XVI, 1952.Google Scholar
54. Lucassen, L. R., Meyer Drees, J. and Senger, E. C. (1948). Emergency Landing After Power Failure with a Sikorsky S. 41 Helicopter. N.L.L. Report V. 1463, 1948.Google Scholar
55. Lucassen, L. R., Meyer Drees, J. and Senger, E. C. (1951). Methods of Testing at Constant Attitude (Polar and Longitudinal Characteristics.) I.C.A.O. Circular 16-AN/13, 1951.Google Scholar
56. Maas, H. J. Van der, Marx, A. J. and Oosterom, T. VAN (1940). Static Lateral Stability, Lateral Control and Control Position Curves in Their Mutual Relations; Their Estimation and Measurement by Means of Flight Tests. N.L.L. Reports and Transactions, Vol. IX, 1940.Google Scholar
57. Linden, J. C. Van der (1954). Equipment for the Measurement of Pressure Distribution in Non-Steady Flight. N.L.L. Report V. 1697, 1954 (in Dutch).Google Scholar
58. Buhrman, J. and Burgerhout, TH. J. (1954). Pressure Distribution on a Wing Section Contour of the S. 14 Machtrainer as Measured in Flight up to a Mach Number of 0-85. N.L.L. Report V. 1654, 1954.Google Scholar
59. Burgerhout, TH. J. (1953). Pressure Distribution on the Cockpit Hood of the S. 14 Machtrainer as measured in Flight. N.L.L. Report V. 1653, 1953 (in Dutch).Google Scholar
60. Linden, J. C. Van der (1954). Description of the Equipment and Method for the Determination of Wing Torsion and Tailplane Deflection of the S. 14 Machtrainer in Flight. N.L.L. Report V. 1655, 1954 (in Dutch).Google Scholar
61. Koiter, W. T. (1943). The Effective Width of Infinitely Long, Flat, Rectangular Plates under Various Conditions of Edge Restraint. N.L.L. Report S. 287, 1943. (Dutch with English Abstract).Google Scholar
62. Koiter, W. T. (1944). Theoretical Investigation of the Diagonal Tension Field of Flat Plates. N.L.L. Report S. 295, 1944 (Dutch with English Abstract).Google Scholar
63. Neut, A. Van der (1948). Experimental Investigation of the Post-Buckling Behaviour of Flat Plates, Loaded in Shear and Compression. N.L.L. Report S. 341, Reports and Transactions, Vol. XV, 1948.Google Scholar
64. Floor, W. K. G. and Burgerhout, T. J. (1952). Evaluation of the Theory on the Post-Buckling Behaviour of Stiffened, Flat, Rectangular Plates Subjected to Shear and Normal Loads. N.L.L. Report S. 370, Reports and Transactions, Vol. XVI, 1952.Google Scholar
65. Floor, W. K. G. (1955). Investigation of the Post- Buckling Effective Strain Distribution in Stiffened, Flat, Rectangular Plates Subjected to Shear and Normal Loads. N.L.L. Report S. 427, Reports and Transactions, Vol. XIX, 1955.Google Scholar
66. Botman, M. and Besseling, J. F. (1955). The Effective Width in the Plastic Range of Flat Plates under Compression. N.L.L. Report S. 445, Reports and Transactions, Vol. XIX, 1955.Google Scholar
67. Botman, M. (1955). The Effective Width in the Plastic Range of Flat Plates under Compression. Part 111. N.L.L. Report S.465, 1955.Google Scholar
68. Koiter, W. T. (1956). Buckling and Post-Buckling Behaviour of a Cylindrical Panel under Axial Compression. N.L.L. Report S. 476, Reports and Transactions, Vol. XX, 1956.Google Scholar
69. Plantema, F. J. (1952). Theory and Experiments on the Elastic Overall Instability of Flat Sandwich Plates. Doctor Thesis, Delft, 1952. (Also N.L.L. Report S. 402, Reports and Transactions, Vol. XVII, 1953.)Google Scholar
70. Plantema, F. J. and Alphen, W. J. Van (1952). Compressive Buckling of Sandwich Plates Having Various Edge Conditions. N.L.L. Report S.404, 1952. C. B. Biezeno Anniv. Vol. on Apvl. Mech., Stam, Haarlem, 1953.Google Scholar
71. Besselino, I. F. (1955). On the Buckling Problem in the Plastic Range for Struts and Plates. Part III. Experiments and Non-Dimensional Buckling Curves. N.L.L. Report S. 444, 1955.Google Scholar
72. Besselino, J. F. (1954). A Theory of Plastic Flow for Anisotropic Hardening in Plastic Deformation of an Initially Isotropic Material. N.L.L. Report S.410, 1954.Google Scholar
73. Floor, W. K. G. (1953). Shear Tests on 24 S-T Unstiffened and Stiffened Webs with Flanged Holes. Part I. N.L.L. Report S.413, 1953.Google Scholar
74. Botman, M. (1955). Shear Tests on 24 S-T Unstiffened and Stiffened Webs with Flanged Holes. Part II. N.L.L. Report S. 446, 1955.Google Scholar
75. Besselino, J. F. and Floor, W. K. G. (1954). Torsional Strength and Stiffness Tests of Wing Leading Edges. N.L.L. Report S. 421, Reports and Transactions, Vol. XVI11, 1954.Google Scholar
76. Neut, A. VAN DER (1953). The Local Instability of Compression Members, Built up from Flat Plates. C. B. Biezeno Anniv. Vol. on Appl. Mech., Stam, Haarlem, 1953.Google Scholar
77. Iacobs, F. A. and Hartman, A. (1954). The Effect of Sheet Thickness and Overlap on the Fatigue Strength at Repeated Tension of Redux Bonded 75 S-T Clad Single Lap loints. N.L.L. Report M. 1969, 1954.Google Scholar
78. Klaassen, W. and Hartman, A. (1955). The Fatigue Diagram for Fluctuating Tension of Single Lap loints of Clad 24 S-T and 75 S-T Aluminum Alloy with 2 Rows of 17 S Rivets. N.L.L. Report M. 1980, 1955.Google Scholar
79. Hartman, A. and Klaassen, W. (1956). The Fatigue Strength at Fluctuating Tension of Single Lap loints of Clad 24 S-T and 75 S-T Aluminum Alloy with 2 Rows of 17 S Rivets. N.L.L.—T.N. M. 2011, 1956.Google Scholar
80. Rondeel, J. H. Kruithof, R. and Plantema, F. J. (1954). Comparative Fatigue Tests with 24 S-T Alclad Riveted and Bonded Stiffened Panels. N.L.L. Reports S. 416, Reports and Transactions, Vol. XVIII, 1954.Google Scholar
81. Hartman, A. and Rondeel, J. H. (1954). Static Tests and Fatigue Tests on Redux Bonded Built-Up and Solid Light Alloy Spar Booms. N.L.L. Report M. 1936, Reports and Transactions, Vol. XIX, 1954.Google Scholar
82. Schijve, J. A. and Jacobs, F.A. (1955). Fatigue Tests on Notched and Unnotched Clad 24 S-T Sheet Specimens to Verify the Cumulative Damage Hypothesis. N.L.L. Report M. 1982, 1955.Google Scholar
83. Plantema, F. J. (1955). Some Investigations on Cumulative Damage. Proc. Colloquium on Fatigue, Stockholm. Springer, 25th-27th May, 1955.Google Scholar
84. Schijve, J. and Jacobs, F. A. (1956). Research on Cumulative Damage in Fatigue on Riveted Aluminum Alloy Joints. N.L.L. Report M. 1999, Reports and Transactions, Vol. XX, 1956.Google Scholar
85. Schijve, J. (1956). Fatigue Crack Propagation in Light Alloys. N.L.L. T.N. M. 2010, 1956.Google Scholar
86. Hartman, A. (1956). Mechanical Properties of Glass Fibre Reinforced Plastics at Room Temperature. N.L.L. Report M. 1991, 1956 (in Dutch).Google Scholar
87. Burgers, J. M. (1924). The Motion of a Fluid in the Boundary Layer Along a Plain Smooth Surface. Proceedings of the First International Congress for Applied Mechanics, Delft, 1924.Google Scholar
88. Malotaux, P. C. A., Dernier van der gon, J. J. and Yap Kie yan, (1951). A Method for Qualitative Boundary-Layer Investigation by Means of Hot Wires Without Disturbing the Flow. Technical University, Report VTH-45, Delft, 1951 (in Dutch with English Summary).Google Scholar
89. Ingen, J. L. Van(1956) A Suggested Semi-Empirical Method for the Calculation of the Boundary-Layer Transition Region. Technical University, Report VTH-74, Delft, 1956.Google Scholar
90. Smith, A. M. O. (1956). Transition, Pressure Gradient and Stability Theory. Lecture Presented at IX International Congress for Applied Mechanics, Brussels, 1956.Google Scholar
91. Dobbinga, E. and Ghesel grothe, J. A. Van (1955). The Low Speed Wind Tunnel of the Department of Aeronautical Engineering of the Technological University at Delft. De Ingenieur, No. 38, 1955 (in Dutch, with English Summary).Google Scholar
92. neut, a. van der (1956). buckling caused by thermal stresses. technical university, report vth-68, delft, 1956.Google Scholar
93. Neut, A. Van der. Post Buckling Performance of Plates under Thermal Load. Technical University, Report VTH-70. Delft (to he Published).Google Scholar