Measurement of the moments of inertia of the Handley Page H. P. 115 aircraft /

Handley Page bombers of the First World War /
by: Bowyer, Chaz
Published: (1992)

Free-flight model measurements of the dynamic stability of a supersonic strike aircraft (TSR2) /
by: Hunt, G. K.
Published: (1967)

Some problems in the automatic control and stability of supersonic transport aircraft /
by: Ruggles, R.
Published: (1970)

Vertical accelerations due to structural vibrations of a slender aircraft flying in continuous turbulence /
by: Zbrozek, J. K.
Published: (1966)

The longitudinal response of a flexible slender aircraft to random trubulence /
by: Huntley, E.
Published: (1967)

The economic effects of meteorological forecasting standards for supersonic civil transports /
by: Courtney, Adrian Laurence
Published: (1969)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8 /
by: Winter, Kenneth George
Published: (1968)

Some flight and wind-tunnel longitudinal stability measurements on the BAC slender-wing aircraft /
by: Barnes, C. S.
Published: (1970)

Handling qualities of aircraft with marginal longitudinal stability /
by: Saunders, T. B.
Published: (1966)

Airflow rate requirements in passenger aircraft /
by: Timby, E. A.
Published: (1970)

Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
by: Shaw, M. M.
Published: (1967)

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

The influence of elevator movement on the normal accelerations experienced by a transport aircraft in moderate turbulence /
by: Eckford, Duncan John
Published: (1969)

Pressure-plotting and force tests at Mach numbers up to 2.8 on an uncambered slender wing of p = 1/2, s/co = 1/4 ('Handley Page Ogee') /
by: Courtney, Adrian Laurence
Published: (1964)

A flight simulation study of the handling characteristics of a slender wing supersonic transport aircraft at landing approach speeds /
by: Perry, D. H. (David Howard)
Published: (1970)

Aircraft stalling and buffeting.
Published: (1975)

Selected papers on advanced design of air vehicles /
by: Ferri, Antonio, 1912-
Published: (1977)

The potential theory of unsteady supersonic flow.
by: Miles, John Wilder
Published: (1959)

Measurements of wing buffeting on a Scimitar model /
by: Mabey, Dennis G.
Published: (1967)

A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach number /
by: Pierce, D.
Published: (1967)

115th Infantry, U.S.A., in the World War.
by: Reynolds, F. C. (Frederick C.)
Published: (1920)

Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight ; Parts I and II /
by: Taylor, A. S.
Published: (1966)

Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model /
by: Cox, A. P.
Published: (1967)

Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds /
by: Isaacs, Donald
Published: (1966)

The dynamic stability derivatives of a slender wing : a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4 /
by: Turner, K. J.
Published: (1968)

Civil supersonic aircraft development (SST) : hearings before a subcommittee of the Committee on Appropriations, House of Representatives, Ninety-second Congress, first session.
Published: (1971)

Cruise data report R/V CHAIN cruise 115, leg 7 /
by: Kroll, J. D.
Published: (1975)

A model for the aquaplaning of tyres on wet runways /
by: Cooke, J. C. (John Caister)
Published: (1969)

Civil supersonic aircraft development (SST) for fiscal year 1971 : hearings, Ninety-second Congress, first session.
Published: (1971)

Anticollision lights for the supersonic transport (SST) /
by: Gerathewohl, Siegfried J. (Siegfried Johannes), 1909-
Published: (1970)

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls /
by: Isaacs, Donald
Published: (1969)

An analogue computer for on-line correction of wind-tunnel force and moment data /
by: Pecover, B. E.
Published: (1967)

A history of Marine Fighter Attack Squadron 115 /
by: Chapin, John C.
Published: (1988)

The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flow /
by: Golesworthy, G. T.
Published: (1967)

Further tests with a variable ramp intake having a design Mach number of 2.2 /
by: Neale, M. C.
Published: (1966)