Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 PDF full book. Access full book title Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 by Edwin J. Saltzman. Download full books in PDF and EPUB format.

Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6

Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 PDF Author: Edwin J. Saltzman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56

Book Description


Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6

Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6 PDF Author: Edwin J. Saltzman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56

Book Description


Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2

Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 PDF Author: Edwin J. Saltzman
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 686

Book Description


X-15 Research Results

X-15 Research Results PDF Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : X-15 (Rocket aircraft).
Languages : en
Pages : 140

Book Description


Supersonic Aerodynamics of Large-angle Cones

Supersonic Aerodynamics of Large-angle Cones PDF Author: James F. Campbell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 84

Book Description


A Reassessment of Heavy-Duty Truck Aerodynamic Design Features and Priorities

A Reassessment of Heavy-Duty Truck Aerodynamic Design Features and Priorities PDF Author: Edwin J. Saltzman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40

Book Description


Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0

Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0 PDF Author: Sheryll Goecke Powers
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44

Book Description


Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1284

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1284

Book Description


Flight-measured Base Pressure Coefficients for Thick Boundary-layer Flow Over an Aft-facing Step for Mach Numbers from 0.4 to 2.5

Flight-measured Base Pressure Coefficients for Thick Boundary-layer Flow Over an Aft-facing Step for Mach Numbers from 0.4 to 2.5 PDF Author: Sheryll A. Goecke
Publisher:
ISBN:
Category : B-70 bomber
Languages : en
Pages : 44

Book Description