Effect of underwing frost on a transport aircraft airfoil at flight Reynolds number (English)
National licence
- New search for: Bragg, M. B.
- New search for: Heinrich, D. C.
- New search for: Valarezo, W. O.
- New search for: McGhee, R. J.
- New search for: Bragg, M. B.
- New search for: Heinrich, D. C.
- New search for: Valarezo, W. O.
- New search for: McGhee, R. J.
In:
Journal of Aircraft
;
31
, 6
;
1372-1379
;
1994
-
ISSN:
- Article (Journal) / Electronic Resource
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Title:Effect of underwing frost on a transport aircraft airfoil at flight Reynolds number
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Contributors:Bragg, M. B. ( author ) / Heinrich, D. C. ( author ) / Valarezo, W. O. ( author ) / McGhee, R. J. ( author )
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Published in:Journal of Aircraft ; 31, 6 ; 1372-1379
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Publisher:
- New search for: The American Institute of Aeronautics and Astronautics
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Publication date:1994-01-01
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Size:8 pages
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ISSN:
-
DOI:
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Type of media:Article (Journal)
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Type of material:Electronic Resource
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Language:English
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Source:
Table of contents – Volume 31, Issue 6
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1233
-
Flow visualization studies on sidewall effects in two-dimensional transonic airfoil testingSudani, Norikazu / Sato, Mamoru / Kanda, Hiroshi / Matsuno, Kenichi et al. | 1994
- 1240
-
Pilot Weather Advisor systemSeth, Shashi / Crabill, Norman L. et al. | 1994
- 1244
-
Progress in high-lift aerodynamic calculationsRogers, Stuart E. et al. | 1994
- 1251
-
Authors: AIAA Journal to be Available on CD-ROM| 1994
- 1252
-
Sidewash on the vertical tail in subsonic and supersonic flowsChiu, Chyn-shan / Lin, I. J. et al. | 1994
- 1257
-
Limit cycle phenomena in computational transonic aeroelasticityKousen, Kenneth A. / Bendiksen, Oddvar O. et al. | 1994
- 1264
-
Polar patrol balloonNishimura, Jun / Yajima, Nobuyuki / Akiyama, Hiromitsu / Ejiri, Masaki / Fujii, Ryoichi / Kokubun, S. et al. | 1994
- 1268
-
Design constraints in the payload-range diagram of ultrahigh capacity transport airplanesMartinez-Val, Rodrigo / Perez, Emilio / Munoz, Tomas / Cuerno, Cristina et al. | 1994
- 1273
-
Computation of the poststall behavior of a circulation controlled airfoilLinton, Samuel W. et al. | 1994
- 1281
-
Experimental Investigation of the Flowfield About an Upswept AfterbodyEpstein, R.J. et al. | 1994
- 1281
-
Experimental investigation of the flowfield about an unswept afterbodyEpstein, Ronald J. / Carbonaro, Mario C. / Caudron, F. et al. | 1994
- 1291
-
Unstructured grid solutions to a wing/pylon/store configurationParikh, Paresh / Pirzadeh, Shahyar / Frink, Neal T. et al. | 1994
- 1297
-
Nonlinear angle of twist of advanced composite wing boxes under pure torsionRomeo, Giulio / Frulla, Giacomo / Busto, Mario et al. | 1994
- 1303
-
Moving wall effect in relation to other dynamic stall flow mechanismsEricsson, Lars E. et al. | 1994
- 1310
-
Ram accelerator ballistic range concept for softly accelerating hypersonic free-flying modelsNaumann, K. W. / Bruckner, Adam P. et al. | 1994
- 1317
-
Separation control on high-lift airfoils via micro-vortex generatorsLin, John C. / Robinson, Stephen K. / McGhee, Robert J. / Valarezo, Walter O. et al. | 1994
- 1324
-
Study of an airfoil with a flap and spoilerAl Shabibi / Abdullah / Al Hammadi / Munir / Mathew, Joseph et al. | 1994
- 1328
-
Stratospheric towed vehicle conceptOckels, Wubbo J. / Melkert, Joris A. / Roelen, Alfred L. C. et al. | 1994
- 1333
-
Navier-Stokes prediction of large-amplitude delta-wing roll oscillationsChaderjian, Neal M. et al. | 1994
- 1341
-
Analysis of a higher harmonic control test to reduce blade vortex interaction noiseBrooks, Thomas F. / Booth, Earl R. / Boyd, D. D. / Splettstoesser, Wolf R. / Schultz, Klaus-J. / Kube, Roland / Niesl, Georg H. / Streby, Olivier et al. | 1994
- 1350
-
Further analysis of high-rate rolling experiments of a 65-deg delta wingEricsson, Lars E. / Hanff, Ernest S. et al. | 1994
- 1358
-
Engineering transition prediction for a hypersonic axisymmetric boundary layerStilla, J. et al. | 1994
- 1365
-
Forebody flow control on a full-scale F/A-18 aircraftLanser, Wendy R. / Meyn, Larry A. et al. | 1994
- 1372
-
Effect of underwing frost on a transport aircraft airfoil at flight Reynolds numberBragg, M. B. / Heinrich, D. C. / Valarezo, W. O. / McGhee, R. J. et al. | 1994
- 1380
-
Pneumatic concept for tip-stall control of cranked-arrow wingsRao, Dhanvada M. et al. | 1994
- 1387
-
Structural acoustic calculations in the low-frequency rangeDe Rosa / S. / Pezzullo, G. / Lecce, L. / Marulo, F. et al. | 1994
- 1395
-
Postinstability Behavior of a Two-Dimensional Airfoil with a Structural NonlinearityPrice, S.J. et al. | 1994
- 1395
-
Poststability behavior of a two-dimensional airfoil with a structural nonlinearityPrice, S. J. / Lee, B. H. K. / Alighanbari, H. et al. | 1994
- 1402
-
Dynamic analysis of bearingless tail rotor blades based on nonlinear shell modelsBauchau, Olivier A. / Chiang, Wuying et al. | 1994
- 1402
-
Dynamic Analysis of Bearingless Tall Rotor Blades Based on Nonlinear Shell ModelsBauchau, O. A. / Chiang, W. et al. | 1994
- 1411
-
Static pressure distribution in the inlet of a helicopter turbine compressorvan der Walt / Johannes P. / Nurick, Alan et al. | 1994
- 1413
-
Static aeroelastic characteristics of a composite wingLee, In / Kim, Seung-Ho / Miura, Hirokazu et al. | 1994
- 1416
-
Experiments on the automatic control of boundary-layer transitionRioual, J.-L. / Nelson, P. A. / Fisher, M. J. et al. | 1994
- 1419
-
Method for the prediction of the onset of wing rockLiebst, Brad S. / Nolan, Robert C. et al. | 1994
- 1422
-
Inverse Solutions of the Prandti-Meyer FunctionOezcan, O. / Edis, F. O. / Aslan, A. R. / Pinar, I. et al. | 1994
- 1422
-
Inverse solutions of the Prandtl-Meyer functionOzcan, O. / Edis, F. O. / Aslan, A. R. / Pinar, I. et al. | 1994
- 1424
-
Flow study of supersonic wing-nacelle configurationBiber, Kasim / Mendoza, Joel et al. | 1994
- 1426
-
Analytic prediction of lift for delta wings with partial leading-edge thrustTraub, Lance W. et al. | 1994
- 1429
-
Computational study of plume-induced separation on a hypersonic powered modelHuebner, L. D. et al. | 1994
- 1431
-
Effect of leeward flow dividers on the wing rock of a delta wingNg, T. T. / Skaff, Tony / Kountz, John et al. | 1994
- 1433
-
Integration of the supersonic kernel functionvan Zyl / Louw H. et al. | 1994
- 1436
-
Redundancy in the discrete-vortex method for closed bodiesSrivastava, Ashok / Mook, Dean T. et al. | 1994
- 1438
-
Subject Index| 1994
- 1446
-
Author Index| 1994
- 1448
-
Chronological Index| 1994