Aircraft strength and stiffness

Aircraft strength and stiffness, Total:63 items.

The international standard classification for "Aircraft strength and stiffness" includes: .

The Chinese standard classification for "Aircraft strength and stiffness" includes: Basic standards and general methods .

Professional Standard - Aviation

HB 7295-1996 Methods and Requirements for Aircraft Strength and Rigidity Ground Test System Calibration

Military Standard of the People's Republic of China-General Armament Department

GJB 67.3-1985 Military aircraft strength and stiffness specifications other loads
GJB 67.6-1985 Military aircraft strength and stiffness specifications, reliability requirements and fatigue loads
GJB 2755-1996 Carrier Aircraft Strength and Stiffness Specification Vibration, Flutter and Divergence
GJB 67.12-1985 Military aircraft strength and stiffness specification documents and reports
GJB 67.5-1985 Military Aircraft Strength and Stiffness Specification Water Loading and Operating Loads for Seaplanes
GJB 2753-1996 Carrier Aircraft Strength and Stiffness Specification Ground Loading
GJB 2751-1996 Carrier Aircraft Strength and Stiffness Specifications Flight Loads
GJB 2757-1996 Carrier-based aircraft strength and stiffness specifications airframe retention
GJB 2752-1996 Carrier Aircraft Strength and Stiffness Specifications Other Loads
GJB 67.10-1985 Military aircraft strength and stiffness specifications flight testing
GJB 67.7-1985 Military Aircraft Strength and Stiffness Specification Aeroelastic Instabilities
GJB 67.9-1985 Ground testing of military aircraft strength and stiffness specifications
GJB 2759-1996 Carrier-based aircraft strength and stiffness specification flight test
GJB 67.4-1985 Military Aircraft Strength and Stiffness Specification Ground Loading
GJB 2756-1996 Carrier-based aircraft strength and stiffness regulate nuclear weapon effects
GJB 2758-1996 Ground testing of carrier-based aircraft strength and stiffness specifications
GJB 67.8-1985 Military Aircraft Strength and Stiffness Specification Vibration
GJB 67.2-1985 Military Aircraft Strength and Stiffness Specification Flight Loading
GJB 2760-1996 Carrier-based aircraft strength and stiffness specification data and reports
GJB 2750-1996 General principles for strength and stiffness specifications for carrier-based aircraft
GJB 67.1-1985 General principles for strength and stiffness specifications for military aircraft

未注明发布机构

GJB 67.13-1990 Military Aircraft Strength and Stiffness Specification Acoustic Fatigue

Korean Agency for Technology and Standards (KATS)

KS W 0624-2013 AIRPLANE STRENGTH AND RIGIDITY, VIBRATION
KS W 0624-2003(2008) AIRPLANE STRENGTH AND RIGIDITY, VIBRATION
KS W 0625-2012 Airplane strength and rigidity, sonic fatigue
KS W 0622-1983 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
KS W 0622-2003(2013) AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
KS W 0619-1981(2009) Airplane strength and rigidify, water and handling loads for seaplanes
KS W 0625-2002(2012) Airplane strength and rigidity, sonic fatigue
KS W 0619-2013 Airplane strength and rigidify, water and handling loads for seaplanes
KS W 0646-1994(2009) Airplane strength and rigidity, flight ground operation tests
KS W 0646-2013 Airplane strength and rigidity, flight ground operation tests
KS W 0624-2003 Airplane strength and rigidity vibration
KS W 0617-1984 Airplane Strength and Rigidity, Flight Loads
KS W 0622-2003 Airplane strength and rigidity ground tests
KS W 0620-1978 Airplane strength and rigidity, miscellaneous loads
KS W 0620-1992 Airplane strength and rigidity, miscellaneous loads
KS W 0623-2013 AIRPLANE STRENGTH AND RIGIDITY, FLUTTER, DIVERGENCE AND OTHER AEROELASTIC INSTABILITIES

United States Navy

NAVY MIL-A-8861 B-1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
NAVY MIL-A-8861 B (1)-1994 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS [Use In Lieu Of: NAVY MIL-A-008861 A CANC NOTICE]
NAVY MIL-A-8867 C-1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
NAVY MIL-A-8867 C (1)-1993 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
NAVY MIL-A-8869 B-1987 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS
NAVY MIL-A-8869 B VALID NOTICE 1-1994 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS [Use In Lieu Of: NAVY MIL-A-008869 A CANC NOTICE 1]
NAVY MIL-A-8870 C-1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
NAVY MIL-A-8867 C VALID NOTICE 1-1994 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS [Use In Lieu Of: NAVY MIL-A-008867 B CANC NOTICE 1]
NAVY MIL-A-8863 C-1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
NAVY MIL-A-8866 C VALID NOTICE 1-1994 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE [Use In Lieu Of: NAVY MIL-A-008866 B CANC NOTICE 1]
NAVY MIL-A-8866 C-1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE

SCC

MIL MIL-A-8861B-1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (SUPERSEDING MIL-A-8861A)
MIL MIL-A-8867C-1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS (SUPERSEDING MIL-A-8867B)
MIL MIL-A-8860B-1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR (SUPERSEDING MIL-A-8860A)
MIL MIL-A-8869B-1987 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS (SUPERSEDING MIL-A-8869A)
MIL MIL-A-8863C-1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (SUPERSEDING MIL-A-8863B)
MIL MIL-A-8870C-1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (SUPERSEDING MIL-A-8870B)
MIL MIL-A-8865B-1987 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS (SUPERSEDING MIL-A-8865 AND MIL-A-008865A)
MIL MIL-A-8870B-1987 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (S/S BY MIL-A-8870C)
MIL MIL-A-8871A-1971 AIRPLANE STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (S/S BY MIL-A-87221)
MIL MIL-A-8868B-1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (NO S/S DOCUMENT) (SUPERSEDING MIL-A-8868A)

Japanese Industrial Standards Committee (JISC)

JIS W 0606:1981 Airplane strength and rigidity, general specification for
JIS W 0607:1984 Airplane strength and rigidity, flight loads

U.S. Air Force

AIR FORCE MIL-A-8860 B-1987 AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR [Use In Lieu Of: AIR FORCE MIL-A-008860 A CANC NOTICE 1] [Superseded: MIL-S-5701 CANC NOTICE 1, MIL-S-5701]

Others: Aircraft strength and stiffness flight and ground handling tests,Drone strength and stiffness,Aircraft Strength and Stiffness Ground Test System Calibration Method and Requirements,Specifications for UAV Strength and Stiffness (Part 1 - Part 11)