Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment - Info and Reading Options
By Perry A Newman
"Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment" was published by National Information Branch in 1984 - Washington, D.C, it has 41 pages and the language of the book is English.
“Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment” Metadata:
- Title: ➤ Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment
- Author: Perry A Newman
- Language: English
- Number of Pages: 41
- Publisher: National Information Branch
- Publish Date: 1984
- Publish Location: Washington, D.C
“Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Testing - Transonic Aerodynamics - Wind tunnels - Winged spacecraft
Edition Specifications:
- Pagination: v, 41 p. :
Edition Identifiers:
- The Open Library ID: OL14933596M - OL11307212W
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