GB9010458D0 - Evaluation of static pressure downstream of a normal shock in hypersonic flight - Google Patents

Evaluation of static pressure downstream of a normal shock in hypersonic flight

Info

Publication number
GB9010458D0
GB9010458D0 GB909010458A GB9010458A GB9010458D0 GB 9010458 D0 GB9010458 D0 GB 9010458D0 GB 909010458 A GB909010458 A GB 909010458A GB 9010458 A GB9010458 A GB 9010458A GB 9010458 D0 GB9010458 D0 GB 9010458D0
Authority
GB
United Kingdom
Prior art keywords
evaluation
static pressure
pressure downstream
normal shock
hypersonic flight
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
GB909010458A
Other versions
GB2243912B (en
GB2243912A (en
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB9010458A priority Critical patent/GB2243912B/en
Publication of GB9010458D0 publication Critical patent/GB9010458D0/en
Publication of GB2243912A publication Critical patent/GB2243912A/en
Application granted granted Critical
Publication of GB2243912B publication Critical patent/GB2243912B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G01P5/17—Coupling arrangements to the indicating device
    • G01P5/175—Coupling arrangements to the indicating device with the determination of Mach number

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Measuring Fluid Pressure (AREA)
GB9010458A 1990-05-10 1990-05-10 Evaluation of static pressure downstream of a normal shock in hypersonic flight Expired - Fee Related GB2243912B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9010458A GB2243912B (en) 1990-05-10 1990-05-10 Evaluation of static pressure downstream of a normal shock in hypersonic flight

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9010458A GB2243912B (en) 1990-05-10 1990-05-10 Evaluation of static pressure downstream of a normal shock in hypersonic flight

Publications (3)

Publication Number Publication Date
GB9010458D0 true GB9010458D0 (en) 1990-07-04
GB2243912A GB2243912A (en) 1991-11-13
GB2243912B GB2243912B (en) 1994-02-23

Family

ID=10675737

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9010458A Expired - Fee Related GB2243912B (en) 1990-05-10 1990-05-10 Evaluation of static pressure downstream of a normal shock in hypersonic flight

Country Status (1)

Country Link
GB (1) GB2243912B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5610845A (en) * 1994-08-30 1997-03-11 United Technologies Corporation Multi-parameter air data sensing technique

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3206974A (en) * 1959-05-06 1965-09-21 Kollsman Instr Corp Integrated flight instrument system
GB893565A (en) * 1959-06-03 1962-04-11 Kelvin & Hughes Ltd Improvements in or relating to computing apparatus
US4319333A (en) * 1979-12-19 1982-03-09 Smiths Industries Limited Mach airspeed indicator

Also Published As

Publication number Publication date
GB2243912B (en) 1994-02-23
GB2243912A (en) 1991-11-13

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940523