Suchergebnisse für ""William D Harkins""

Base Pressure and Static Pressure for a Cone-cylinder at a Nominal Mach Number of 5.8.
18,99 €
Versandfertig in über 4 Wochen
William D Harkins
Base Pressure and Static Pressure for a Cone-cylinder at a Nominal Mach Number of 5.8.
  (Aktuell noch keine Bewertungen)
Broschiertes Buch
9. September 2021
Creative Media Partners, LLC
Papers on Smelter Smoke, [acute Arsenical Poisoning]
20,99 €
Versandfertig in über 4 Wochen
William D Harkins
Robert Eccles Swain
Papers on Smelter Smoke, [acute Arsenical Poisoning]
  (Aktuell noch keine Bewertungen)
Broschiertes Buch
19. Februar 2018
Creative Media Partners, LLC
Intermediate and Complex Ions. V. The Solubility Product and Activity of the Ions in Bi-valent Salt ..
30,99 €
Versandfertig in über 4 Wochen
Versandkostenfrei*
William D Harkins
H M Paine
Intermediate and Complex Ions. V. The Solubility Product and Activity of the Ions in Bi-valent Salt ..
  (Aktuell noch keine Bewertungen)
Gebundenes Buch
6. Dezember 2015
Creative Media Partners, LLC

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Boundary Layer Temperature Recovery Factor on a Cone at Nominal Mach Number Six.
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Boundary Layer Temperature Recovery Factor on a Cone at Nominal Mach Number Six.
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An Experimental Investigation of Flow Over Simple Blunt Bodies at a Mach Number of 5.8.
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An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.
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An Experimental Investigation by Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.
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An Experimental Investigation by Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.
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Effect of Mach Number on Position Error as Applied to a Pitot-static Tube Located 0.55 Chord Ahead of an Airplane Wing
16,99 €
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Effect of Mach Number on Position Error as Applied to a Pitot-static Tube Located 0.55 Chord Ahead of an Airplane Wing
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Impact Pressure and Total Temperature Interpretation at Hypersonic Mach Number.
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Jack C Graves
Impact Pressure and Total Temperature Interpretation at Hypersonic Mach Number.
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Interaction Between Shock Waves and Turbulent or Transitional Boundary Layers at Mach Number 3.
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Edelbert E Irish
Interaction Between Shock Waves and Turbulent or Transitional Boundary Layers at Mach Number 3.
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An Investigation of the Effect of a Laminar Body Boundary Layer on the Body Interference Pressures of a Wing-body Combination at Mach Number 1.9
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An Investigation of the Effect of a Laminar Body Boundary Layer on the Body Interference Pressures of a Wing-body Combination at Mach Number 1.9
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An Investigation of the Variation of Elevator Power and Damping in Pitch With Mach Number for an FJ-3B Fury Jet Airplane Through Steady State Flight Tests
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An Investigation of the Variation of Elevator Power and Damping in Pitch With Mach Number for an FJ-3B Fury Jet Airplane Through Steady State Flight Tests
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Broschiertes Buch
9. September 2021
Creative Media Partners, LLC
An Experimental Investigation of the Effects Upon Lift of a Gap Between Wing and Body of a Slender Wing-body Combination at Mach Number 1.9.
17,99 €
Versandfertig in über 4 Wochen
An Experimental Investigation of the Effects Upon Lift of a Gap Between Wing and Body of a Slender Wing-body Combination at Mach Number 1.9.
  (Aktuell noch keine Bewertungen)
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9. September 2021
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