Abstract
On December 17, 1937, B. Melvill Jones presented the first Wright Brothers’ lecture at Columbia University in New York (Ref. 1). His lecture, which was entitled “Flight Experiments on the Boundary Layer,” dealt specifically with the first British flight observations of transition of the boundary layer from laminar to turbulent flow. These data, Jones concluded, showed that it is possible to retain a laminar layer over at least one-third of the whole wing surface even when the chord Reynolds number is as high as 8 millions. In the 50 years since this presentation, much flight research has been performed to explore the potential of laminar flow control for drag reduction. Both passive control and active control by suction (designated as natural laminar flow and laminar flow control, respectively) have been researched and impressive results achieved. The successes of the early natural laminar flow (NLF) flight testing were remarkable, with the achievement of an extent of laminar flow and transition Reynolds numbers which were not to be exceeded in flight for over 40 years. Nevertheless, mid-century manufacturing capabilities were such that insufficiently smooth or wave-free wing surfaces led to failure of attempts to transfer this technology to practice. The experience with laminar. flow control (LFC) nearly paralleled that of NLF.
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Abbreviations
- TACT:
-
Transonic aircraft technology
- NACA:
-
National Advisory Committee on Aeronautics
- NPL:
-
National Physics Laboratory
- LFC:
-
Laminar flow control
- mac:
-
Mean aerodynamic chord
- LTPT:
-
Low-Turbulence Pressure Tunnel
- Max:
-
Maximum
- PW:
-
Pratt and Whitney
- NLF:
-
Natural laminar flow
- LE, TE:
-
Leading edge, trailing edge
- OASPL:
-
Overall sound pressure level
- rpm:
-
Revolutions per minute
- dB:
-
Decibel
- N-OASPL:
-
Normalized overall sound pressure level
- Hz.:
-
Hertz
- HLFC:
-
Hybrid laminar flow control
- Alt.:
-
Altitude
References
Jones, B. M.: Flight Experiments on the Boundary Layer. JAS, Vol. 5, No. 3, pp. 81–94. January 1938.
Whites, R. C.; Sudderth, R. W.; and Wheldon, W. G.: Laminar Flow Control on the X-21. Astronautics and Aeronautics, Vol. 4, No. 7, July 1966.
Wagner, R. D.; and Fischer, M. C.: Developments in the NASA Transport Aircraft Laminar Flow Program. AIAA-83–0090, January 1983.
Wetmore, J. W.; Zalovcik, J. A.; and Platt, R. C.: A Flight Investigation of the Boundary-Layer Characteristics and Profile Drag of the NACA 35–215 Laminar-Flow Airfoil at High Reynolds Numbers. NACA L-532, 1941.
von Doenhoff, A. E.; and Braslow, A. L.: Effect of Distributed Surface Roughness on Laminar Flow. Chapter of Boundary Layer and Flow Control-Its Principles and Applications, Volume 2, edited by G. V. Lachmann, Pergamon Press, New York, 1961.
Braslow, A. L.: Investigation of Effects of Various Camouflage Paints and Painting Procedures on the Drag Characteristics of an NACA 65(421)-420, a = 1.0 Airfoil Section. NACA CB No. L4G17, July 1944.
Braslow, A. L.; and Visconti, F.: Investigation of Boundary-Layer Reynolds Number for Transition on an NACA 65(215)114 Airfoil in the Langley Two-Dimensional Low-Turbulence Pressure Tunnel NACA TN 1704, October 1948.
Gray, W. E.; and Fullam, P. W. J.: Comparison of Flight and Tunnel Measurements of Transition on a Highly Finished Wing (King Cobra). RAE Report Aero 2383, 1945.
Smith, F.; and Higton, D.: Flight Tests on King Cobra FZ.440 to Investigate the Practical Requirements for the Achievement of Low Profile Drag Coefficients on a “Low Drag” Aerofoil. R and M 2375, British A.R.C., 1950.
Plascoff, R. H.: Profile Drag Measurements on Hurricane II z. 3687 Fitted with Low-Drag Section Wings. RAE Report No. Aero 2153, 1946.
Zalovcik, J. A.; Wetmore, J. W.; and von Doenhoff, A. E.: Flight Investigation of Boundary-Layer Control by Suction Slots on an NACA 35–215 Low-Drag Airfoil at High Reynolds Numbers. NACA WR L-521, 1944.
Head, M. R.: The Boundary Layer With Distributed Suction. R and M No. 2783, British A. R. C., 1955.
Head, M. R.; Johnson, D.; and Coxon, M.: Flight Experiments on Boundary Layer Control for Low Drag. R and M No. 3025, British A. R. C., March 1955.
Edwards, B.: Laminar Flow Control - Concepts, Experiences, Speculations. AGARD Report No. 654. Special Course on Concepts for Drag Reduction, 1977.
Pfenninger, W.; Groth, E. E.; Whites, R. C.; Carmichael, B. H.; and Atkinson, J. M.: Note About Low Drag Boundary Layer Suction Experiments in Flight on a Wing Glove of a F94-A Airplane. Reference No. NAI-54–849 (BLC-69), Northrop Aircraft, Inc., December 1954.
Pfenninger, W.: Laminar Flow Control Laminarization. In Special Course on Concepts for Drag Reduction, AGARD-R654, June 1977.
Landeryou, R. R.; and Porter, P. G.: Further Tests of a Laminar Flow Swept Wing with Boundary Layer Control by Suction. Report Aero. No. 192, College of Aeronautics, Cranfield (England), May 1966.
Gray, W. E.: The Effect of Wing Sweep on Laminar Flow, RAE TM Aero. 255, 1952.
Anscombe, A.; and Illingworth, L. N.: Wind Tunnel Observations of Boundary Layer Transition on a Wing at Various Angles of Sweepback. R and M No. 2968, British A. R. C., 1956.
Pfenninger, W.; Gross, L.; and Bacon, J. W., Jr.: Experiments on a 30 Degree Swept, 12 Percent Thick, Symmetrical, Laminar Suction Wing in the 5-Foot by 7-Foot Michigan Tunnel Northrop Corp., Norair Division Report. NAI-57–317 (BLC93), February 1957.
Boeing Commercial Airplane Company: Natural Laminar Flow Airfoil Analysis and Trade Studies, NASA CR-159029. May 1979.
Steers, L. L.: Natural Laminar Flow Flight Experiment. NASA CP-2172, pp. 135–144, October 1980.
Montoya, L. C.; Steers, L. L.; Christopher, D.; Trujillo, B.: F111 TACT Natural Laminar Flow Glove Flight Results. NASA CP-2208, pp. 11–20, September 1981.
Boeing Commercial Airplane Company: F-111 Natural Laminar Flow Glove Flight Test Data Analysis and Boundary-Layer Stability Analysis. NASA CR-166051. January 1984.
Runyan, L. J.; and Steers, L. L.: Boundary-Layer Stability Analysis of a Natural Laminar Flow Glove on the F-111 TACT Airplane, Viscous Flow Drag Reduction, Vol. 72, Progress in Astronautics and Aeronautics, pp. 17–32, 1980.
Rozendaal, R. A.: Variable Sweep Transition Flight Experiment (VSTFE) - Parametric Pressure Distribution, Boundary-Layer Stability Study and Wing Glove Design Task. NASA CR-3992, 1986.
Waggoner, E. G.; Campbell, R. L.; Phillips, P. S.; and Hallissy, J. B.: Design and Test of an NLF Glove Wing for the Variable Sweep Transition Flight Experiment. NASA CP-2487, pp. 753–776, 1987.
Wagner, R. D.; Maddalon, D. V.; Bartlett, D. W.; Collier, F. S. Jr.; and Braslow, A. L.: Laminar Flow Flight Experiments. From Proceedings of the Transonic Aerodynamics Symposium held at NASA Langley Research Center. NASA CP 3020, 1988.
Bohn-Meyer, M.: Constructing Gloved Wings for Aerodynamic Studies, AIAA 88–2109, May 1988.
Meyer, R. R.; Trujillo, B. M.; and Bartlett, D. W.: F-14 VSTFE and Results of the Cleanup Flight Test Program. NASA CP-2487, pp. 819–844, 1987.
Boeing Commercial Airplane Company: Flight Survey of the 757 Wing Noise Field and Its Effect on Laminar Boundary Layer Transition. NASA CR-178216, Vol. I - Program Description and Data Analysis. March 1987.
Boeing Commercial Airplane Company: Flight Survey of the 757 Wing Noise Field and Its Effect on Laminar Boundary Layer Transition. NASA CR-178217, Vol. 2 - Data Compilation. March 1987.
Boeing Commercial Airplane Company: Flight Survey of the 757 Wing Noise Field and Its Effect on Laminar Boundary Layer Transition. NASA CR-178419, Vol. 3 - Extended Data Analysis. May 1988.
Boltz, F. W.; Kenyon, G. C.; and Allen, C. Q.: Effects of Sweep Angle on the Boundary-Layer Stability Characteristics of an Untapered Wing at Low Speeds. NASA TN D-338, 1960.
Malik, M. R.: Cosal-A Black Box Compressible Stability Anal-ysis Code for Transition Prediction in Three-Dimensional Boundary Layers. NASA CR-165925, 1982.
Malik, M. R.; and Poll, D. I. A.: Effect of Curvature on Three-Dimensional Boundary Layer Stability. AIAA Journal, Vol. 23, No. 9, pp. 1362–1369. September 1985.
Collier, F. S., Jr.; and Malik, M. R.: Stationary Disturbances in Three-Dimensional Boundary Layers. AIAA Paper 87–1412, June 1987.
Collier, F. S., Jr.: Curvature Effects on the Stability of Three-Dimensional Laminar Boundary Layers. Ph.D. Dissertation, Virginia Polytechnic Institute and State University, May 1988.
Mack, L. M.: Boundary Layer Stability Theory. AGARD Report No. 709, Special Course on Stability and Transition of Laminar Flows, VKI, Brussels, 1984.
Swift, G; and Mangur P.: A Study of the Prediction of Cruise Noise and Laminar Flow Control Noise Criteria for Subsonic Air Transports. NASA CR-159104, August 1979.
Douglas Aircraft Company Staff: Laminar Flow Control Leading Edge Glove Flight Test Article Development. NASA CR172137, 1984.
Etchberger, F. R.: Laminar Flow Control Leading Edge Glove Flight Aircraft Modification Design, Test Article Development, and Systems Integration. NASA CR-172136, 1983.
Fisher, D. F.; and Fischer, M. C.: The Development Flight Tests of the JetStar LFC Leading-Edge Flight Experiment. NASA CP-2487, pp. 117–140, 1987.
Maddalon, D. V.; Fisher, D. F.; Jennett, L. A.; and Fischer, M. C.: Simulated Airline Service Experience with Laminar Flow Control Leading-Edge Systems. NASA CP-2487, pp. 195–218, 1987.
Powell, A. G.; and Varner, L. D.: The Right Wing of the LEFT Airplane. NASA CP-2487, pp. 141–161, 1987.
Davis, R. E.; Maddalon, D. V.; and Wagner, R. D.: Performance of Laminar Flow Leading Edge Test Articles in Cloud Encounters. NASA CP-2487, pp. 163–193, 1987.
Goodyear, M. D.: Application of Superplastically Formed and Diffusion Bonded Aluminum to a Laminar Flow Control Leading Edge. NASA CR-178316, 1987.
Jasperson, W. H.; Nastrom, G. D.; Davis, R. E.; and Holde-man, J. D: GASP Cloud - and Particle Encounter Statistics, and Their Application to LFC Aircraft Studies (2 Vols.). NASA TM 85835, October 1984.
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© 1992 Springer-Verlag New York, Inc.
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Wagner, R.D., Maddalon, D.V., Bartlett, D.W., Collier, F.S., Braslow, A.L. (1992). Laminar Flow Flight Experiments — A Review. In: Barnwell, R.W., Hussaini, M.Y. (eds) Natural Laminar Flow and Laminar Flow Control. ICASE/NASA LaRC Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-2872-1_2
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