Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115) /
| Main Author: | Bisgood, P. L. |
|---|---|
| Other Authors: | O'Leary, C. O. |
| Format: | Book |
| Language: | English |
| Published: |
London :
H.M.S.O.,
1966.
|
| Series: | Current papers (Aeronautical Research Council (Great Britain)) ;
no. 838. |
| Subjects: |
Similar Items
Measurement of the moments of inertia of the Handley Page H. P. 115 aircraft /
by: Fennell, L. J.
Published: (1967)
by: Fennell, L. J.
Published: (1967)
A piloted simulator study of a slender-wing research aircraft (HP 115) /
by: McPherson, A.
Published: (1970)
by: McPherson, A.
Published: (1970)
The Handley Page type 42 commercial airplane (British) : a metal sesquiplane.
Published: (1930)
Published: (1930)
Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)
The lateral oscillation of slender aircraft /
by: Ross, A. Jean
Published: (1966)
by: Ross, A. Jean
Published: (1966)
The aerodynamic effect of ground proximity on lateral control of slender aircraft in the landing approach /
by: Pinsker, W. J. G.
Published: (1971)
by: Pinsker, W. J. G.
Published: (1971)
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)
by: Perry, D. H. (David Howard)
Published: (1970)
The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)
by: Mabey, Dennis G.
Published: (1968)
Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
by: Shaw, M. M.
Published: (1967)
by: Shaw, M. M.
Published: (1967)
'Zero rate of climb speed' as a low speed limitation for the stall-free aircraft /
by: Pinsker, W. J. G.
Published: (1967)
by: Pinsker, W. J. G.
Published: (1967)
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)
by: Isaacs, Donald
Published: (1969)
Handley Page bombers of the First World War /
by: Bowyer, Chaz
Published: (1992)
by: Bowyer, Chaz
Published: (1992)
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)
by: Winter, Kenneth George
Published: (1968)
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)
by: Cox, A. P.
Published: (1967)
Flight determination of the rudder power and directional stability of the Fairey Delta 2 aircraft using a wingtip parachute /
by: Ingle, G.
Published: (1974)
by: Ingle, G.
Published: (1974)
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)
by: Courtney, Adrian Laurence
Published: (1964)
Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight ; Parts I and II /
by: Taylor, A. S.
Published: (1966)
by: Taylor, A. S.
Published: (1966)
Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)
by: Harris, G. Z.
Published: (1967)
Some flight and wind-tunnel longitudinal stability measurements on the BAC slender-wing aircraft /
by: Barnes, C. S.
Published: (1970)
by: Barnes, C. S.
Published: (1970)
Results and analysis of pressure measurements on two isolated slender wings and slender wing-body combinations at supersonic speeds /
by: Fellows, K. A.
Published: (1970)
by: Fellows, K. A.
Published: (1970)
Vertical accelerations due to structural vibrations of a slender aircraft flying in continuous turbulence /
by: Zbrozek, J. K.
Published: (1966)
by: Zbrozek, J. K.
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)
by: Turner, K. J.
Published: (1968)
Measurements of buffeting on slender wing models /
by: Mabey, Dennis G.
Published: (1967)
by: Mabey, Dennis G.
Published: (1967)
Boundary layer separation in a centrebody nozzle with parallel shroud /
by: Herbert, M. V., et al.
Published: (1966)
by: Herbert, M. V., et al.
Published: (1966)
The longitudinal response of a flexible slender aircraft to random trubulence /
by: Huntley, E.
Published: (1967)
by: Huntley, E.
Published: (1967)
The design of a series of warped slender wings for subsonic speeds /
by: Davies, Patricia J.
Published: (1974)
by: Davies, Patricia J.
Published: (1974)
Numerical studies on hypersonic delta wings with detached shock waves /
by: Shanbhag, V. V.
Published: (1974)
by: Shanbhag, V. V.
Published: (1974)
The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)
Low-speed wind-tunnel measurements of the oscillatory lateral aerodynamic derivatives of a BAC 221 model and comparison of results with similar Concorde and HP 115 Data /
by: O'Leary, C. O.
Published: (1971)
by: O'Leary, C. O.
Published: (1971)
A review of recent research on handling qualities, and its application to the handling problems of large aircraft /
by: Bisgood, P. L.
Published: (1967)
by: Bisgood, P. L.
Published: (1967)
Selected papers on advanced design of air vehicles /
by: Ferri, Antonio, 1912-
Published: (1977)
by: Ferri, Antonio, 1912-
Published: (1977)
Tests on an engine installation for a slender gothic wing at M-1.82 /
by: Griffiths, R. T.
Published: (1967)
by: Griffiths, R. T.
Published: (1967)
Measurements of wing buffeting on a Scimitar model /
by: Mabey, Dennis G.
Published: (1967)
by: Mabey, Dennis G.
Published: (1967)
The dynamic stability derivatives of a slender wing at zero and moderate lift : a comparison of theory with free-flight model tests, M = 0.8 to 2.0 /
by: Ross, A. Jean, et al.
Published: (1975)
by: Ross, A. Jean, et al.
Published: (1975)
Flight and tunnel measurements of pressure fluctuations on the upper surface of the wing of a Venom aircraft with a sharpened leading-edge /
by: Rose, R. (Robert), et al.
Published: (1969)
by: Rose, R. (Robert), et al.
Published: (1969)
Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speeds /
by: Britton, J. W.
Published: (1967)
by: Britton, J. W.
Published: (1967)
Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing /
by: Griffiths, R. T.
Published: (1969)
by: Griffiths, R. T.
Published: (1969)
A method of correlating the ground effects on the longitudinal characteristics of slender wings /
by: Kirkpatrick, David L. I.
Published: (1970)
by: Kirkpatrick, David L. I.
Published: (1970)
Some calculations of the take-off behaviour of a slender-wing supersonic transport design constrained to follow a specified pitch-attitude time history /
by: Tomlinson, Barry Nigel
Published: (1967)
by: Tomlinson, Barry Nigel
Published: (1967)
Free-flight model measurements of the dynamic stability of a supersonic strike aircraft (TSR2) /
by: Hunt, G. K.
Published: (1967)
by: Hunt, G. K.
Published: (1967)