Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads, John T. Batina

Resource Information

The instance Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads, John T. Batina represents a material embodiment of a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries. This resource is a combination of several types including: Instance, Microform.

Label

Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads, John T. Batina

Statement of responsibility

John T. Batina

Instantiates

• Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads

Publication

• Washington, D.C., National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985

Base of film

safety base undetermined

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

233591644

Dimensions

4x6 in. or 11x15 cm.

Extent

1 volume.

Form of item

microfiche

Generation

service copy

Media category

microform

Media MARC source

rdamedia

Media type code

• h

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

n 85-18957

Positive negative aspect

negative

Record ID

.b64341847

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

02

ReductionRatioRange

normal reduction

Reproduction note

Microfiche.

Specific material designation

microfiche