Opening book details…
About this nonfiction
Stability and Control Characteristics at a Mach Number of 1.89 of a Lightweight Glider Reentry Configuration by Robinson, Ross B. is a nonfiction available to read on EtoBox.
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Robinson, Ross B.
- Publisher
- National Aeronautics and Space Administration, 1960.
- Published
- 1960
- Language
- EN
- Category
- nonfiction
More by Robinson, Ross B.
Browse all works by Robinson, Ross B.
Similar books
- Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration — Gerald V. Foster (1959)
- Static Longitudinal Stability Characteristics of a Blunted Glider Reentry Configuration Having 79.5° Sweepback and 45° Dihedral at Mach Number of 6.2 and Angles of Attack Up to 20° — Edward E. Mayo (1959)
- Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90° — John E. Grimaud (1961)
- Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70° Delta Wing — Driver, Cornelius. (1960)
- Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings — Gerald V. Foster (1960)
- An Investigation of the Dynamic Stability and Control Characteristics for a Transport Cruising at a Mach Number of 3 — Lawrence W. Brown (1964)