Results 101 to 110 of about 101,352 (285)

Design of F-16 Airfoil Mock-ups for Supersonic Wind Tunnel: Study, Production, Testing and Validation

, 2023
N. Eddegdag, A. Naamane, M. Radouani
openalex   +2 more sources

Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 deg to 15 deg [PDF]

Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 ...
Howell, D. T., Stallings, R. L., Jr.
core   +1 more source

A mechanics model in design of flexible nozzle with multiple movable hinge boundaries. [PDF]

Heliyon, 2023
Yu C, Li Z, Zhang Z, Meng L, Wang G, Shi Y, Gao C.   +6 more
europepmc   +1 more source

Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel [PDF]

A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 Foot Supersonic/9 by 15 Foot Low speed Wind Tunnel.
Arrington, E. Allen, Pickett, Mark T.
core   +1 more source

Langley 50th anniversary [PDF]

, 1967
Summary of Langley Research Center accomplishments in aeronautics and astronautics during past fifty ...

core   +1 more source

Gust Generator for a Supersonic Wind Tunnel [PDF]

The effectiveness was investigated of a flat plate gust generator that was located in the nozzle throat of the Lewis 10- by 10-foot supersonic wind tunnel. Gust plates were tested at nozzle wall Mach numbers of 3.1, 2.4, and 2.0.
Bishop, Allan R., Sanders, Bobby W., Webb, John A., Jr.   +2 more
core   +1 more source

Aerodynamics Caused by Rolling Rates of a Small-Scale Supersonic Flight Experiment Vehicle with a Cranked-Arrow Main Wing

Aerospace
A small-scale supersonic flight experiment vehicle is being developed at Muroran Institute of Technology as a flying testbed for verification of innovative technologies for high-speed atmospheric flights, which are essential to next-generation aerospace ...
Kazuhide Mizobata, Koji Shirakata, Atsuya Honda, Keisuke Shiono, Yukiya Ishigami, Akihiro Nishida, Masaaki Miura   +6 more
doaj   +1 more source

An Investigation of the Lift, Drag, and Pitching Moment Characteristics of AGARD Calibration Model B in N.A.L. 1m×1m Supersonic Blowdown Wind Tunnel.

, 1963
Hiroharu TAKAGI, Takashi Tani, Hideo Saitô, Kiyoshi Arai   +3 more
openalex   +2 more sources

Supersonic Flutter of Conical Shells: II Wind Tunnel Tests

, 1977
上田 哲彦, 紀平 正知, 小林 繁夫   +2 more
openalex   +2 more sources

Transatmospheric vehicle research [PDF]

Research was conducted into the alternatives to the supersonic combustion ramjet (scramjet) engine for hypersonic flight. A new engine concept, the Oblique Detonation Wave Engine (ODWE) was proposed and explored analytically and experimentally.
Adelman, Henry G., Cambier, Jean-Luc
core   +1 more source