Pressure Distribution

147 books
Environment, inequality, and collective actionM. Franzini
⏱ 4h 12m

Environment, inequality, and collective action

M. Franzini

2005252 pp.
Politicians, Legislation, and the EconomyR. E. McCormick

Politicians, Legislation, and the Economy

R. E. McCormick

1981No page data
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validationRobert S. Jankovsky
⏱ 51m

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

Robert S. Jankovsky

199951 pp.
Evaluation of 3D inverse code using rotor 67 as test caseT. Dang

Evaluation of 3D inverse code using rotor 67 as test case

T. Dang

1998No page data
Pressure distributions for the GA(W)-2 airfoil with 20% aileron, 25% slotted flap and 30% Fowler flapW. H. Wentz
⏱ 1h 21m

Pressure distributions for the GA(W)-2 airfoil with 20% aileron, 25% slotted flap and 30% Fowler flap

W. H. Wentz

197881 pp.
The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnelNorbert Ulbrich
⏱ 3h 6m

The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel

Norbert Ulbrich

1998186 pp.
Laser scanning system for pressure and temperature paintsJohn Sullivan

Laser scanning system for pressure and temperature paints

John Sullivan

1997No page data
Pressures inside a room subjected to sonic boomNabil Naguib Wahba

Pressures inside a room subjected to sonic boom

Nabil Naguib Wahba

1977No page data
Response of a flexibly supported string to a convected random pressure fieldP. H. White
⏱ 1h 6m

Response of a flexibly supported string to a convected random pressure field

P. H. White

196266 pp.
Direct calculation of airfoils from pressure distributionRichard Eppler
⏱ 1h 1m

Direct calculation of airfoils from pressure distribution

Richard Eppler

197461 pp.
Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoilerW. H. Wentz
⏱ 1h 52m

Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler

W. H. Wentz

1979112 pp.
Analysis of two-phase flow in damper seals for cryogenic turbomachineryGrigory L. Arauz

Analysis of two-phase flow in damper seals for cryogenic turbomachinery

Grigory L. Arauz

1996No page data
Rocket-based combined cycle engine technology developmentJ. R. DeBonis

Rocket-based combined cycle engine technology development

J. R. DeBonis

1996No page data
Wake measurements in a strong adverse pressure gradientR. Hoffenberg

Wake measurements in a strong adverse pressure gradient

R. Hoffenberg

1995No page data
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stallR. A. Piziali
⏱ 9h 19m

2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

R. A. Piziali

1994559 pp.
Age, class, politics, and the welfare stateFred C. Pampel
⏱ 3h 19m

Age, class, politics, and the welfare state

Fred C. Pampel

1989199 pp.
Improved two-equation k - [omega] turbulence models for aerodynamic flowsFlorian R. Menter

Improved two-equation k - [omega] turbulence models for aerodynamic flows

Florian R. Menter

1992No page data
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler codeWendy B. Lessard
⏱ 1h 17m

Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code

Wendy B. Lessard

199677 pp.
Enhanced design of turbo-jet LPT by separation control using phased plasma actuatorsThomas C. Corke

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

Thomas C. Corke

2003No page data
Effects of winglets on a first-generation jet transport wingRobert R. Meyer
⏱ 56m

Effects of winglets on a first-generation jet transport wing

Robert R. Meyer

198656 pp.
Page 1 of 8Next →