Opening book details…
About this nonfiction
Dynamic response of a forward-swept-wing model at angles of attack up to 15 at a Mach number of 0.8 by Doggett, Robert V. 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
- Doggett, Robert V.
- Publisher
- National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1980.
- Published
- 1980
- Language
- EN
- Category
- nonfiction
More by Doggett, Robert V.
Browse all works by Doggett, Robert V.
Similar books
- Wind-tunnel experiments on divergence of forward-swept wings / Rodney H. Ricketts and Robert V. Doggett, Jr. — Rodney H. Ricketts (1980)
- Pressures and heat transfer on a 75 ̊swept delta wing with trailing-edge flap at Mach 6 and angles of attack to 90 J. Wayne Keyes. — Keyes, J. Wayne. (1969)
- Effect of Skewed Wing-tip Controls on a Highly Swept Arrow Wing at Mach Number 2.03 — Landrum, Emma Jean. (1964)
- Sweeping Forward: Developing & Flight Testing the Grumman X-29A Forward Swept Wing Research Aircraft — Frederick A. Johnsen
- Subsonic Longitudinal and Lateral-directional Characteristics of a Forward-swept-wing Fighter Configuration at Angles of Attack Up to 470 / Michael J. Mann, Jarrett K. Huffman, and Charles H. Fox, Jr. — Michael J. Mann (1987)
- Pressure Measurements of the Leading Edge of a Swept Wing at Mach 2.2 — Russell B. Sorrells (1974)