CA719523A - High speed axial flow compressors - Google Patents

High speed axial flow compressors

Info

Publication number
CA719523A
CA719523A CA719523A CA719523DA CA719523A CA 719523 A CA719523 A CA 719523A CA 719523 A CA719523 A CA 719523A CA 719523D A CA719523D A CA 719523DA CA 719523 A CA719523 A CA 719523A
Authority
CA
Canada
Prior art keywords
high speed
axial flow
flow compressors
speed axial
compressors
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA719523A
Inventor
T. Forster Vincent
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
English Electric Co Ltd
Original Assignee
English Electric Co Ltd
Publication date
Application granted granted Critical
Publication of CA719523A publication Critical patent/CA719523A/en
Expired legal-status Critical Current

Links

CA719523A High speed axial flow compressors Expired CA719523A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA719523T

Publications (1)

Publication Number Publication Date
CA719523A true CA719523A (en) 1965-10-12

Family

ID=36055100

Family Applications (1)

Application Number Title Priority Date Filing Date
CA719523A Expired CA719523A (en) High speed axial flow compressors

Country Status (1)

Country Link
CA (1) CA719523A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3989406A (en) * 1974-11-26 1976-11-02 Bolt Beranek And Newman, Inc. Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3989406A (en) * 1974-11-26 1976-11-02 Bolt Beranek And Newman, Inc. Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like

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