Deflection of turbofan exhaust streams for enhanced engine/nacelle integration

Journal of Aircraft

Volumn 35, Issue 1, 1998, Pages 106-112

  Tindell, R H ^a,d,g   Marconi, F ^a,d,g   Kalkhoran, I ^b,e,g   Yetter, J ^c,f  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b POLYTECHNIC UNIVERSITY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d BAE Systems Advanced Systems and Technologies   (United States)

^e Mech Engineering and Aeronautics

^f Component Integration Branch ^*

^g AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CASCADES (FLUID MECHANICS); JETS; MATHEMATICAL MODELS; NOZZLES; NUMERICAL ANALYSIS; THRUST REVERSAL; TURBOFAN ENGINES;

ENGINE/NACELLE INTEGRATION; EULER ANALYSIS; FAN FLOW DEFLECTION; THRUST VECTORING;

EXHAUST SYSTEMS (ENGINE);

EID: 0031678752     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2266     Document Type: Article

References (5)

1. Vetter, J. A., "Why Do Airlines Want and Use Thrust Reversers?" NASA TM 109158, Jan. 1995.
2. Tindell, R., "Experimental Evaluation of the Blockerless Thrust Reverser Concept," Northrop Grumman, Rept. ATDC 95-105, April 1995.
3. "Thrust Reverser," Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, Paris, France, Publication, April 1954.
4. Abramovich, G. N., The Theory of Turbulent Jets, MIT Press, Cambridge, MA, 1963, pp. 365-370.
5. Federspiel, J., Bangert, L., Wing, D., and Hawks, T., "Fluidic Control of Nozzle Flow - Some Performance Measurements," AIAA Paper 95-2605, July 1995.