On the effect of altitude upon the distance required for an aircraft to take off and climb 20 metres, giving generalised curves of weight reduction necessary if a given aircraft is to comply with the requirements of A.P. 1208 under adverse atmospheric conditions
By: by K.T. Spencer.
Series: Aeronautical research committee -- 1307
Publisher: His Majesty's Stationery Office
Published: 1930
Place of publication: London
Language: eng
Subjects: Airplanes -- Landing.; Airplanes -- Take-off.
Notes: At the head of the title: Aeronautical research committee.