Aerodynamic Balance

19 books
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8ê to 90êUnknown Author

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8ê to 90ê

Unknown Author

1979No page data
Dynamic stability instrumentation system (DSIS)Unknown Author

Dynamic stability instrumentation system (DSIS)

Unknown Author

1994No page data
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰J. N. Ralston

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰

J. N. Ralston

1984No page data
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8 ̊to 90 ̊Unknown Author

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8 ̊to 90 ̊

Unknown Author

1979No page data
A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectorsKenneth H. Goodrich
⏱ 24m

A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors

Kenneth H. Goodrich

198924 pp.
Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊William Bihrle
⏱ 7h 23m

Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊

William Bihrle

1978443 pp.
Techniques for measurement of dynamic stability derivatives in ground test facilitiesClarence John Schueler
⏱ 3h 29m

Techniques for measurement of dynamic stability derivatives in ground test facilities

Clarence John Schueler

1967209 pp.
X-38 vehicle 131 flutter assessmentJames P. Smith - undifferentiated
⏱ 23m

X-38 vehicle 131 flutter assessment

James P. Smith - undifferentiated

199723 pp.
Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flightG. H. Gaonkar

Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight

G. H. Gaonkar

1996No page data
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰ to 90⁰Unknown Author

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰ to 90⁰

Unknown Author

1984No page data
Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30ê to 90êWilliam Bihrle
⏱ 7h 23m

Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30ê to 90ê

William Bihrle

1978443 pp.
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8 ̊to 90 ̊Unknown Author

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8 ̊to 90 ̊

Unknown Author

1979No page data
Effect of control surface mass unbalance on the stability of a closed-loop active control systemE. Nissim

Effect of control surface mass unbalance on the stability of a closed-loop active control system

E. Nissim

1989No page data
An analogue computer for on-line correction of wind-tunnel force and moment dataB. E. Pecover
⏱ 24m

An analogue computer for on-line correction of wind-tunnel force and moment data

B. E. Pecover

196724 pp.
A review of ice accretion data from a model rotor icing test and comparison with theoryRandall K. Britton

A review of ice accretion data from a model rotor icing test and comparison with theory

Randall K. Britton

1991No page data
Applications of magnetic suspension technology to large scale facilitiesColin P. Britcher

Applications of magnetic suspension technology to large scale facilities

Colin P. Britcher

1997No page data
Mass balancing of hollow fan bladesRobert E. Kielb

Mass balancing of hollow fan blades

Robert E. Kielb

1986No page data
Application of magnetic suspension and balance systems to ultra-high Reynolds number facilitiesColin P. Britcher

Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities

Colin P. Britcher

1996No page data
Divergence analysis report for the bodies of revolution model support systemsLarry C. Rash

Divergence analysis report for the bodies of revolution model support systems

Larry C. Rash

1983No page data