FR2316122A1 - Dispositif a voilure tournante - Google Patents

Dispositif a voilure tournante

Info

Publication number
FR2316122A1
FR2316122A1 FR7619803A FR7619803A FR2316122A1 FR 2316122 A1 FR2316122 A1 FR 2316122A1 FR 7619803 A FR7619803 A FR 7619803A FR 7619803 A FR7619803 A FR 7619803A FR 2316122 A1 FR2316122 A1 FR 2316122A1
Authority
FR
France
Prior art keywords
wing
dynamically
longitudinal axis
balanced out
wing segments
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
FR7619803A
Other languages
English (en)
Other versions
FR2316122B3 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wave Rider Inc
Original Assignee
Wave Rider Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wave Rider Inc filed Critical Wave Rider Inc
Publication of FR2316122A1 publication Critical patent/FR2316122A1/fr
Application granted granted Critical
Publication of FR2316122B3 publication Critical patent/FR2316122B3/fr
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/003Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/008Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a longitudinal axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
FR7619803A 1975-06-30 1976-06-29 Dispositif a voilure tournante Granted FR2316122A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US59183575A 1975-06-30 1975-06-30
US67251376A 1976-03-31 1976-03-31

Publications (2)

Publication Number Publication Date
FR2316122A1 true FR2316122A1 (fr) 1977-01-28
FR2316122B3 FR2316122B3 (fr) 1979-03-23

Family

ID=27081274

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7619803A Granted FR2316122A1 (fr) 1975-06-30 1976-06-29 Dispositif a voilure tournante

Country Status (3)

Country Link
JP (1) JPS527597A (fr)
DE (1) DE2627393A1 (fr)
FR (1) FR2316122A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01114685A (ja) * 1987-10-29 1989-05-08 Mitsubishi Electric Corp 断熱構造体

Also Published As

Publication number Publication date
JPS527597A (en) 1977-01-20
DE2627393A1 (de) 1977-02-03
FR2316122B3 (fr) 1979-03-23

Similar Documents

Publication Publication Date Title
CA1111823A (fr) Aeronef a voilure mobile
GB1530620A (en) Airplane-like kite toy
FR2316122A1 (fr) Dispositif a voilure tournante
SE8106271L (sv) Flygplan med arrangemang for montering av en sond
GB1187035A (en) Aerial Guided Missiles with Fins.
US1671225A (en) Toy aeroplane
GB1230760A (fr)
FR2374928A2 (fr) Jouet volant
ZHELUDEV Bending flutter of rotating elongated bodies(Effect of longitudinal acceleration and angular velocity around longitudinal axis on elastic bending vibrations of elongated body of revolution in supersonic flow)
ES131643U (es) Paneles para la construcción de cámara frigoríficas
WALKER Fin design with ACT in the presence of strakes
Savage A short low-speed wind tunnel with wide angle diffusers
ES131742U (es) Juguete mecánico
ALLEGRE et al. Influence of the effects of rarefaction and of angle of attack on a three-dimensional obstacle placed in a rarefied hypersonic flow(Rarefaction and angle of attack effects on delta wing in hypersonic flow in wind tunnel)
FR2354921A1 (fr) Profil d'aile d'aerodyne a geometrie variable
IL53347A0 (en) Tubular projectile adapted to be launched at supersonic velocity
KRONE Flight demonstrations and the forward swept wing
GILLY et al. Determination of the flow upstream of a hemispherical obstacle placed at zero incidence in a current of a perfect fluid at supersonic speed(Flow characteristics behind detached shock wave of hemispherical obstacle placed at zero incidence in current of perfect fluid at supersonic speed)
MASLENNIKOV Determination of the position of sonic points on the head shock wave and on the surface of a blunt body in ballistic investigations(Position determination of sonic points on head shock wave and blunt body surface in ballistics showing Mach number and gas type effects)
FR1075203A (fr) Hélicoptère rotatif gyroscopique avec traction universelle, réacteur spécial, girouette de direction et fusée
CHUSHKIN et al. Three-dimensional supersonic equilibrium flow of a gas around bodies at the angle of attack(Three-dimensional supersonic flow of gas in thermodynamic equilibrium around body at angle of attack)
FR1605383A (en) Guided missile with variable rate of spin - has tail unit with angle of incidence adjustable to vary spinning speed and spring loaded
FR2397982A1 (fr) Aile volante motorisee
HAMMER et al. Research on rudders in a supersonic jetstream
ES246064U (es) Helicoptero de juguete,perfeccionado