Study of the integration of wind tunnel and computational methods for aerodynamic configurations, Lindsay E. Browne and Dale L. Ashby

Resource Information

The instance Study of the integration of wind tunnel and computational methods for aerodynamic configurations, Lindsay E. Browne and Dale L. Ashby represents a material embodiment of a distinct intellectual or artistic creation found in Missouri University of Science & Technology Library. This resource is a combination of several types including: Instance, Microform.

Label

Study of the integration of wind tunnel and computational methods for aerodynamic configurations, Lindsay E. Browne and Dale L. Ashby

Statement of responsibility

Lindsay E. Browne and Dale L. Ashby

Instantiates

• Study of the integration of wind tunnel and computational methods for aerodynamic configurations

Publication

• Moffett Field, Calif., National Aeronautics and Space Administration, Ames Research Center, Springfield, Va., For sale by the National Technical Information Service, 1989

Note

• Shipping list no.: 90-0561-M
• "October 1989."
• "Performing organization report no.: A-89148"--Technical rept. documentation p

Base of film

safety base undetermined

Bibliography note

Includes bibliographical references (page 43)

Carrier category

microfiche

Carrier category code

• he

Carrier MARC source

rdacarrier

Color

black and white

Content category

text

Content type code

• txt

Content type MARC source

rdacontent

Control code

25300351

Dimensions

4x6 in. or 11x15 cm.

Emulsion on film

diazo

Extent

vi, 66 pages

Form of item

microfiche

Generation

service copy

Media category

microform

Media MARC source

rdamedia

Media type code

• h

Other physical details

illustrations.

http://library.link/vocab/ext/overdrive/overdriveId

n 90-13332

Positive negative aspect

negative

Record ID

.b55865574

http://bibfra.me/vocab/marc/reductionRatio

02

ReductionRatioRange

normal reduction

Reproduction note

Microfiche.

Specific material designation

microfiche