Flight Measurements of Some of the Flying Qualities and Stability Derivatives of a Supersonic Fighter Airplane/Detail

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Flight Measurements of Some of the Flying Qualities and Stability Derivatives of a Supersonic Fighter Airplane

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Author and Affiliation:
Champine, R. A.(NASA Langley Research Center, Hampton, VA, United States);
Kraft, C. C., Jr.(NASA Langley Research Center, Hampton, VA, United States);
Mc Laughlin, M. D.(NASA Langley Research Center, Hampton, VA, United States);
White, J. A.(NASA Langley Research Center, Hampton, VA, United States)
Abstract:

Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter aircraft

Publication Date:

Dec 01, 1958

Document ID:


19660024788 (Acquired Feb 12, 1996)


Accession Number:

66N34078

Subject Category:

AIRCRAFT

Report/Patent Number:

NASA-MEMO-10-7-58L

Document Type:

Technical Report

Publisher Information:

United States

Financial Sponsor:

NASA; United States

Organization Source:

NASA Langley Research Center; Hampton, VA, United States

Description:

85p; In English

Distribution Limits:

Unclassified; Publicly available; Unlimited

Rights:

No Copyright

NASA Terms:

DYNAMIC STABILITY; FIGHTER AIRCRAFT; FLIGHT CHARACTERISTICS; FLIGHT TESTS; IN-FLIGHT MONITORING; MEASURING INSTRUMENTS; STABILITY DERIVATIVES; SUPERSONIC AIRCRAFT

Other Descriptors:

DYNAMIC STABILITY; FIGHTER AIRCRAFT; FLIGHT TEST; FLYING QUALITY; SUPERSONIC AIRCRAFT

Imprint And Other Notes:

WASHINGTON, NASA, DEC. 1958 85 P REFS

Miscellaneous Notes:

DECLASSIFIED