Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6 PDF Download

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Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6

Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6 PDF Author: Leo T. Chauvin
Publisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 26

Book Description


Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6

Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6 PDF Author: Leo T. Chauvin
Publisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 26

Book Description


Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6

Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6 PDF Author: Leo T. Chauvin
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

Book Description


Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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Languages : en
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Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.

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Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

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Category : Aerodynamics
Languages : en
Pages : 46

Book Description


Pressures and Heat Transfer on a 75 ̊swept Delta Wing with Trailing-edge Flap at Mach 6 and Angles of Attack to 90

Pressures and Heat Transfer on a 75 ̊swept Delta Wing with Trailing-edge Flap at Mach 6 and Angles of Attack to 90 PDF Author: J. Wayne Keyes
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 52

Book Description
Pressure and heat transfer on swept delta wing with trailing-edge flap.