Performance Evaluation of Transonic Axial Flow Compressor under Distorted Conditions by Groove Casing Technique with Tip Injection and Surface Roughness Effects
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
2250-0553
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
online resource.
- Erschienen in
-
Performance Evaluation of Transonic Axial Flow Compressor under Distorted Conditions by Groove Casing Technique with Tip Injection and Surface Roughness Effects ; volume:103 ; number:4 ; day:11 ; month:6 ; year:2022 ; pages:895-911 ; date:8.2022
Journal of the Institution of Engineers (India) / C. Series C / Institution of Engineers, India / Karnataka State Centre ; 103, Heft 4 (11.6.2022), 895-911, 8.2022
- Urheber
-
Srinivas, G.
Raghunandana, K.
Shenoy, B. Satish
- Beteiligte Personen und Organisationen
-
SpringerLink (Online service)
- DOI
-
10.1007/s40032-022-00851-7
- URN
-
urn:nbn:de:101:1-2022100219412738383380
- Rechteinformation
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
15.08.2025, 07:25 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Srinivas, G.
- Raghunandana, K.
- Shenoy, B. Satish
- SpringerLink (Online service)
Ähnliche Objekte (12)
Axial transonic compressor performance enhancement with circumferential grooves
Circumferential groove casing treatments in centrifugal compressor aerodynamics
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
Influence of Blade Geometry on Secondary Flow Development in a Transonic Centrifugal Compressor
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
Surface roughness of real operationally used compressor blade and blisk
Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls
Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count
Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls
Electrically driven, Compact, Transonic Mixed-Flow Compressor for Active High-Lift Systems in Future Aircraft
Axial transonic compressor performance enhancement with circumferential grooves
Circumferential groove casing treatments in centrifugal compressor aerodynamics
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
Influence of Blade Geometry on Secondary Flow Development in a Transonic Centrifugal Compressor
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
Surface roughness of real operationally used compressor blade and blisk
Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls
Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count
Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls
Electrically driven, Compact, Transonic Mixed-Flow Compressor for Active High-Lift Systems in Future Aircraft
Axial transonic compressor performance enhancement with circumferential grooves
Circumferential groove casing treatments in centrifugal compressor aerodynamics
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
Influence of Blade Geometry on Secondary Flow Development in a Transonic Centrifugal Compressor
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
Surface roughness of real operationally used compressor blade and blisk
Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls
Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count
Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls