"Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds" - Information and Links:

Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds - Info and Reading Options


“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Metadata:

  • Title: ➤  Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
  • Author:

“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Subjects and Themes:

Edition Identifiers:

  • The Open Library ID: OL11563850W

AI-generated Review of “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds”:


Read “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds”:

Read “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” by choosing from the options below.

Search for “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” downloads:

Visit our Downloads Search page to see if downloads are available.

Find “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” in Libraries Near You:

Read or borrow “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” from your local library.

Buy “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” online:

Shop for “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” on popular online marketplaces.


Related Books

Related Editons

Books Results

Source: The Open Library

Editions

Some editions of this work of literature - the Open Library.

1Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Metadata:

  • Title: ➤  Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
  • Language: English
  • Number of Pages: 115
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va

“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Subjects and Themes:

Edition Specifications:

  • Format: Microform
  • Pagination: vi, 115 p.

Edition Identifiers:

Online Marketplaces

Find Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds at online marketplaces:


Top of Page

Find "Wind Tunnel Pressure Study And Euler Code Validation Of A Missile Configuration With 77 ̊swept Delta Wings At Supersonic Speeds" in Wikipdedia