The Resource Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others]
Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others]
Resource Information
The item Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others] represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.This item is available to borrow from 1 library branch.
Resource Information
The item Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others] represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.
This item is available to borrow from 1 library branch.
- Language
- eng
- Extent
- volumes.
- Note
-
- Distributed to depository libraries in microfiche
- Shipping list no.: 94-0429-M
- Contents
-
- v. 1. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 603 ft/sec
- v. 2. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 710 ft/sec
- v. 3. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 603 ft/sec
- v. 4. Laser velocimeter wake data, advance ratio of 0.37
- Label
- Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight
- Title
- Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight
- Statement of responsibility
- W. Derry Mace ... [and others]
- Language
- eng
- Cataloging source
- GPO
- Government publication
- federal national government publication
- Index
- no index present
- Literary form
- non fiction
- http://library.link/vocab/relatedWorkOrContributorName
-
- Mace, W. Derry
- Langley Research Center
- Series statement
- NASA technical memorandum
- Series volume
- 109040, v. 1-<4>
- http://library.link/vocab/subjectName
-
- Laser Doppler velocimeter
- Rotors (Helicopters)
- Label
- Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others]
- Note
-
- Distributed to depository libraries in microfiche
- Shipping list no.: 94-0429-M
- Carrier category
- microfiche
- Carrier category code
- he
- Carrier MARC source
- rdacarrier
- Content category
- text
- Content type code
- txt
- Content type MARC source
- rdacontent
- Contents
- v. 1. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 603 ft/sec -- v. 2. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 710 ft/sec -- v. 3. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 603 ft/sec -- v. 4. Laser velocimeter wake data, advance ratio of 0.37
- Control code
- 17274984
- Extent
- volumes.
- Form of item
- microfiche
- Media category
- microform
- Media MARC source
- rdamedia
- Media type code
- h
- Reproduction note
- Microfiche.
- Stock number
-
- N 94-26483
- N 94-26489
- N 94-26492
- N 94-26497
- Label
- Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others]
- Note
-
- Distributed to depository libraries in microfiche
- Shipping list no.: 94-0429-M
- Carrier category
- microfiche
- Carrier category code
- he
- Carrier MARC source
- rdacarrier
- Content category
- text
- Content type code
- txt
- Content type MARC source
- rdacontent
- Contents
- v. 1. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 603 ft/sec -- v. 2. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 710 ft/sec -- v. 3. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 603 ft/sec -- v. 4. Laser velocimeter wake data, advance ratio of 0.37
- Control code
- 17274984
- Extent
- volumes.
- Form of item
- microfiche
- Media category
- microform
- Media MARC source
- rdamedia
- Media type code
- h
- Reproduction note
- Microfiche.
- Stock number
-
- N 94-26483
- N 94-26489
- N 94-26492
- N 94-26497
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/portal/Investigation-of-the-aerodynamic-environment-for/gDBEO6eMtAI/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/portal/Investigation-of-the-aerodynamic-environment-for/gDBEO6eMtAI/">Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight, W. Derry Mace ... [and others]</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
